1586 lines
78 KiB
Properties
1586 lines
78 KiB
Properties
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#
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# Czech base translation file
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#
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# Should you need to add new logical keys here is the proposed method
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#
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# className.ComponentType.componentName
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#
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#
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# Text tokens within braces should not be translated, e.g.
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# "The file '{filename}' exists."
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# They are pieces that are inserted dynamically.
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#
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! Set to the name of the current translation file (used for debugging purposes)
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debug.currentFile = messages_cs.properties
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! RocketActions
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RocketActions.checkbox.Donotaskmeagain = Pr<EFBFBD>\u0161te se me neptejte
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RocketActions.lbl.Youcanchangedefop = Mu\u017Eete zmenit v<>choz<6F> operaci v nastaven<65>.
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RocketActions.showConfirmDialog.lbl1 = Chcete smazat oznacenou simulaci?
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RocketActions.showConfirmDialog.lbl2 = <html><i>Tuto operaci nelze vz<76>t zpet.</i>
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RocketActions.showConfirmDialog.title = Sma\u017E simulace
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RocketActions.DelCompAct.Delete = Sma\u017E
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RocketActions.DelCompAct.ttip.Delete = Sma\u017E oznacenou komponentu.
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RocketActions.DelSimuAct.Delete = Sma\u017E
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RocketActions.DelSimuAct.ttip.Delete = Sma\u017E oznacenou simulaci.
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RocketActions.DelAct.Delete = Sma\u017E
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RocketActions.DelAct.ttip.Delete = Sma\u017E vyznacenou komponentu nebo simulaci.
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RocketActions.CutAction.Cut = Vyjmout
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RocketActions.CutAction.ttip.Cut = Vyjmi tuto komponentu nebo simulaci do schr<68>nky a odeber z n<>vrhu
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RocketActions.CopyAct.Copy = Copy
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RocketActions.CopyAct.ttip.Copy = Zkopiruj tuto komponentu (a subkomponenty) do schr<68>nky.
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RocketActions.PasteAct.Paste = Paste
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RocketActions.PasteAct.ttip.Paste = Paste the component or simulation on the clipboard to the design.
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RocketActions.EditAct.Edit = Edit
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RocketActions.EditAct.ttip.Edit = Edituj vybranou komponentu.
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RocketActions.NewStageAct.Newstage = Nov<EFBFBD> stupen
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RocketActions.NewStageAct.ttip.Newstage = Pridej nov<6F> stupen rakety.
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RocketActions.ActBoosterstage = Urychlovac<EFBFBD> stupen
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RocketActions.MoveUpAct.Moveup = Presun nahoru
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RocketActions.MoveUpAct.ttip.Moveup = Presun tento stupen smerem nahoru.
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RocketActions.MoveDownAct.Movedown = Presun dolu
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RocketActions.MoveDownAct.ttip.Movedown = Presun tuto komponentu smerem dolu.
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! RocketPanel
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RocketPanel.FigTypeAct.Sideview = Pohled ze strany
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RocketPanel.FigTypeAct.ttip.Sideview = Pohled ze strany
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RocketPanel.FigTypeAct.Backview = Zpetn<EFBFBD> pohled
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RocketPanel.FigTypeAct.ttip.Backview = Zadn<EFBFBD> pohled
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RocketPanel.FigViewAct.2D = 2D Pohled
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RocketPanel.FigViewAct.ttip.2D = 2D Pohled
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RocketPanel.FigViewAct.3D = 3D Pohled
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RocketPanel.FigViewAct.ttip.3D = 3D Pohled
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RocketPanel.lbl.Motorcfg = Nastaven<EFBFBD> motoru:
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RocketPanel.lbl.infoMessage = <html>Stiskni k oznacen<65> Shift+stisknut<75> my\u0161i k oznacen<65> ostatn<74>ch Dvojklik my\u0161i k editov<6F>n<EFBFBD> k editov<6F>n<EFBFBD> Kliknout a t<>hnout k presunu
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! BasicFrame
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BasicFrame.SimpleFileFilter1 = V\u0161echny n<>vrhy raket (*.ork; *.rkt)
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BasicFrame.SimpleFileFilter2 = N<EFBFBD>vrhy OpenRocket (*.ork)
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BasicFrame.SimpleFileFilter3 = N<EFBFBD>vrhy RockSim (*.rkt)
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BasicFrame.tab.Rocketdesign = N<EFBFBD>vrh rakety
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BasicFrame.tab.Flightsim = Letov<EFBFBD> simulace
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BasicFrame.title.Addnewcomp = Pridej novou komponentu
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BasicFrame.dlg.lbl1 = N<EFBFBD>vrh '
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BasicFrame.dlg.lbl2 = ' nebyl ulo\u017Een.
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BasicFrame.dlg.lbl3 = Chcete ho ulo\u017Eit?
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BasicFrame.dlg.title = N<EFBFBD>vrh nen<65> ulo\u017Een
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BasicFrame.StageName.Sustainer = Udr\u017Eet
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BasicFrame.WarningDialog.txt1 = N<EFBFBD>sleduj<EFBFBD>c<EFBFBD> probl<62>my byly zaznamen<65>ny behem otev<65>r<EFBFBD>n<EFBFBD>.
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BasicFrame.WarningDialog.txt2 = Nekter<EFBFBD> prvky nebyly spr<70>vne nahr<68>ny.
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BasicFrame.WarningDialog.title = Varov<EFBFBD>n<EFBFBD> behem otev<65>r<EFBFBD>n<EFBFBD> souboru
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! General error messages used in multiple contexts
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error.fileExists.title = Soubor existuje
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error.fileExists.desc = Soubor '{filename}' existuje. Preejete si ho prepsat?
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error.writing.title = Chyba z<>pisu do souboru
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error.writing.desc = Chyba nastala behem zapisov<6F>n<EFBFBD> do souboru:
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! Labels used in buttons of dialog windows
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# TODO: Rename these to "btn.xxx"
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button.ok = OK
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button.cancel = Zru\u0161it
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button.close = Zavr<EFBFBD>t
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! Common labels used in buttons of dialog windows
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dlg.but.ok = OK
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dlg.but.cancel = Zru\u0161it
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dlg.but.close = Zavr<EFBFBD>t
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! General file type names
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filetypes.pdf = Soubory PDF
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! About Dialog
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AboutDialog.lbl.version = Version
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! The texts below provide additional credits for the translation maintainer
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! - In AboutDialog.lbl.translation replace "English" with the current language.
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! - AboutDialog.lbl.translator is the translator / group name (may be empty)
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! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
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! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
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AboutDialog.lbl.translation = Do ce\u0161tiny prelo\u017Eil:
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AboutDialog.lbl.translator = Vladim<EFBFBD>r Beran
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AboutDialog.lbl.translatorWebsite =
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AboutDialog.lbl.translatorIcon =
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! Print dialog
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PrintDialog.title = Vytisknout nebo exportovat
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PrintDialog.but.previewAndPrint = N<EFBFBD>hled & Tisk
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PrintDialog.checkbox.showByStage = Uka\u017E na sc<73>ne
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PrintDialog.lbl.selectElements = Zvolte polo\u017Eky k prid<69>n<EFBFBD>:
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printdlg.but.saveaspdf = Ulo\u017E jako PDF
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printdlg.but.preview = N<EFBFBD>hled
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printdlg.but.settings = Nastaven<EFBFBD>
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PrintDialog.error.preview.title = Nemohu otevr<76>t n<>hled
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PrintDialog.error.preview.desc1 = Nemohu otevr<76>t PDF N<>hled.
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PrintDialog.error.preview.desc2 = Pros<EFBFBD>m pou\u017Eijte volbu "Ulo\u017Eit jako PDF".
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!PrintSettingsDialog
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PrintSettingsDialog.title = Nastaven<EFBFBD> tisku
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PrintSettingsDialog.lbl.Templatefillcolor = \u0160ablona - barva v<>plne:
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PrintSettingsDialog.lbl.Templatebordercolor = \u0160ablona - barva okraju:
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PrintSettingsDialog.lbl.Papersize = Velikost pap<61>ru:
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PrintSettingsDialog.lbl.Paperorientation = Orientace str<74>nky:
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PrintSettingsDialog.but.Reset = Reset
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PrintSettingsDialog.but.Close = Zavr<EFBFBD>t
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! Bug Report dialog
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bugreport.dlg.title = Hl<EFBFBD>\u0161en<65> chyb
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bugreport.dlg.but.Sendbugreport = Po\u0161li hl<68>\u0161en<65> chyb
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bugreport.dlg.but.Sendbugreport.Ttip = Automaticky pos<6F>lat hl<68>\u0161en<65> o chyb<79>ch v<>voj<6F>rum OpenRocket.
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bugreport.dlg.successmsg1 = Hl<EFBFBD>\u0161en<65> o chybe bylo <20>spe\u0161ne odesl<73>no.
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bugreport.dlg.successmsg2 = Dekujeme, \u017Ee pom<6F>h<EFBFBD>te vylep\u0161ovat OpenRocket!
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bugreport.dlg.successmsg3 = Hl<EFBFBD>\u0161en<65> o chybe
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bugreport.dlg.connectedInternet = <html>Pokud jste pripojeni k internetu stac<61> kliknout na tlac<61>tko <em>Po\u0161li hl<68>\u0161en<65> o chybe</em>.
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bugreport.dlg.otherwise = jinak po\u0161lete n<>sleduj<75>c<EFBFBD> text na adresu:
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bugreport.lbl.Theinformation = Tato informace mu\u017Ee b<>t zahrnuta do verejn<6A>ho hl<68>\u0161en<65> chyb. D<>vejte pozor, aby neobsahovala duvern<72> informace kter<65> si neprejete zverejnit.
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bugreport.dlg.failedmsg1 = OpenRocket nen<65> schopen poslat hl<68>\u0161en<65> o chybe:
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bugreport.dlg.failedmsg2 = Pros<EFBFBD>m po\u0161lete hl<68>\u0161n<31> rucne do:
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bugreport.dlg.failedmsg3 = Chyba behem odes<65>l<EFBFBD>n<EFBFBD> hl<68>\u0161en<65>
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bugreport.reportDialog.txt = <html><b>Mu\u017Eete nahl<68>sit chyby v programu OpenRocket vyplnen<65>m a odesl<73>n<EFBFBD>m formul<75>re.</b><br>Mu\u017Eete tak<61> nahl<68>sit chyby na str<74>nce projektu.
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bugreport.reportDialog.txt2 = <html><b>Pros<6F>m podejte kr<6B>tkou zpr<70>vu o tom co jste delali kdy\u017E chyba nastala.</b>
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bugreport.dlg.provideDescription = Pros<EFBFBD>m poskytnete nejprve hl<68>\u0161en<65> o chybe.
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bugreport.dlg.provideDescription.title = Chyb<EFBFBD> popis chyby
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! Debug log dialog
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debuglogdlg.but.clear = Sma\u017E
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debuglogdlg.OpenRocketdebuglog = Hl<EFBFBD>\u0161en<65> o chybe v OpenRocket
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debuglogdlg.Displayloglines = Zobraz r<>dky z chybov<6F>ho hl<68>\u0161en<65>:
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debuglogdlg.Follow = N<EFBFBD>sleduj
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debuglogdlg.col.Time = Cas
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debuglogdlg.col.Level = <EFBFBD>roven
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debuglogdlg.col.Location = Um<EFBFBD>sten<EFBFBD>
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debuglogdlg.col.Message = Zpr<EFBFBD>va
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debuglogdlg.lbl.Loglinenbr = Z<EFBFBD>znam c<>sla r<>dky:
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debuglogdlg.lbl.Time = Cas:
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debuglogdlg.lbl.Level = <EFBFBD>roven:
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debuglogdlg.lbl.Location = Um<EFBFBD>sten<EFBFBD>:
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debuglogdlg.lbl.Logmessage = Zpr<EFBFBD>va z<>znamu:
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debuglogdlg.lbl.Stacktrace = Tracov<EFBFBD>n<EFBFBD> z<>sobn<62>ku:
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! Edit Motor configuration dialog
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edtmotorconfdlg.but.removemotor = Odeber motor
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edtmotorconfdlg.but.Selectmotor = Vyber motor
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edtmotorconfdlg.but.Removeconfiguration = Odeber nastaven<65>
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edtmotorconfdlg.but.Newconfiguration = Nov<EFBFBD> nastaven<65>
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edtmotorconfdlg.lbl.Motormounts = <html><b>Pripojen<65> motoru:</b>
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edtmotorconfdlg.title.Editmotorconf = <EFBFBD>prava nastaven<65> motoru
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edtmotorconfdlg.selectcomp = <html>Vyber ke kter<65>m komponent<6E>m se m<> motor pripojit:
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edtmotorconfdlg.lbl.Motorconfig = <html><b>Nastaven<65> motoru:</b>
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edtmotorconfdlg.lbl.Configname = Jm<EFBFBD>no nastaven<65>:
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edtmotorconfdlg.lbl.Leavenamedefault = Nechej pr<70>zdn<64> pol<6F>cko jako v<>choz<6F> hodnotu.
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! Example design dialog
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exdesigndlg.but.open = Otevri
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exdesigndlg.lbl.Selectexample = Vyber uk<75>zkov<6F> n<>vrh k otevren<65>:
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exdesigndlg.lbl.Openexampledesign = Otevri uk<75>zkov<6F> n<>vrh
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exdesigndlg.lbl.Exampledesignsnotfound = Uk<EFBFBD>zkov<EFBFBD> n<>vrch nebyl nalezen.
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exdesigndlg.lbl.Examplesnotfound = Uk<EFBFBD>zky nebyly nalezeny
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! Material edit panel
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matedtpan.but.new = Nov<EFBFBD>
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matedtpan.but.edit = Edituj
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matedtpan.but.delete = Sma\u017E
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matedtpan.but.revertall = Vr<EFBFBD>tit v\u0161e zpet
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matedtpan.col.Material = Materi<EFBFBD>l
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matedtpan.col.Type = Typ
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matedtpan.col.Density = Hustota
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matedtpan.col.but.ttip.New = Pridej nov<6F> materi<72>l
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matedtpan.title.Addcustmaterial = Pridej vlastn<74> materi<72>l
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matedtpan.but.ttip.edit = Edituj existuj<75>c<EFBFBD> materi<72>l
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matedtpan.title.Editmaterial = Edituj materi<72>l
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matedtpan.title2.Editmaterial = Vestaven<EFBFBD> materi<72>ly nemohou b<>t modifikov<6F>ny.
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matedtpan.but.ttip.delete = Sma\u017E u\u017Eivatelem definovan<61> materi<72>ly
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matedtpan.but.ttip.revertall = Sma\u017E v\u0161echny u\u017Eivatelem definovan<61> materi<72>ly
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matedtpan.title.Deletealluser-defined = Smazat v\u0161echny u\u017Eivatelem definovan<61> materi<72>ly?
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matedtpan.title.Revertall = Vr<EFBFBD>tit v\u0161e zpet?
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matedtpan.lbl.edtmaterials = Editov<EFBFBD>n<EFBFBD> materi<72>lu neovlivn<76> existuj<75>c<EFBFBD> n<>vrhy raket.
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!MaterialModel
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MaterialModel.title.Material = Materi<EFBFBD>l
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MaterialModel.title.Defcustmat = Definuj vlastn<74> materi<72>l
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! Preference dialog
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pref.dlg.but.add = Pridej
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pref.dlg.but.reset = Reset
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pref.dlg.but.checknow = Zkontroluj nyn<79>
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pref.dlg.but.defaultmetric = V<EFBFBD>choz<EFBFBD> metrick<63> soustava
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pref.dlg.but.defaultimperial = V<EFBFBD>choz<EFBFBD> imperi<72>ln<6C> soustava
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pref.dlg.title.Preferences = Nastaven<EFBFBD>
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pref.dlg.tab.Units = Jednotky
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pref.dlg.tab.Defaultunits = V<EFBFBD>choz<EFBFBD> jednotky
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pref.dlg.tab.Materials = Materi<EFBFBD>ly
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pref.dlg.tab.Custommaterials = Vlastn<EFBFBD> materi<72>ly
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pref.dlg.tab.Options = Vlastnosti
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pref.dlg.tab.Miscellaneousoptions = Ruzn<EFBFBD> vlastnosti
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pref.dlg.lbl.Positiontoinsert = Pozice kam pridat nov<6F> komponenty tela:
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pref.dlg.lbl.Confirmdeletion = Potvrdte smaz<61>n<EFBFBD> simulace:
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pref.dlg.lbl.User-definedthrust = U\u017Eivatelem definovan<61> prubehy v<>konu:
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pref.dlg.Allthrustcurvefiles = Soubory v\u0161ech v<>konov<6F>ch prubehu (*.eng; *.rse; *.zip; directories)
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pref.dlg.RASPfiles = RASPov<EFBFBD> soubory motoru (*.eng)
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pref.dlg.RockSimfiles = RockSim sobory motoru (*.rse)
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pref.dlg.ZIParchives = ZIP archivy (*.zip)
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pref.dlg.checkbox.Checkupdates = Zkontrolujte softwarov<6F> aktualizace pri startu
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|
|
pref.dlg.ttip.Checkupdatesnow = Zkontrolujte softwarov<6F> aktualizace nyn<79>
|
|||
|
|
pref.dlg.lbl.Selectprefunits = Vyberte preferovan<61> jednotky:
|
|||
|
|
pref.dlg.lbl.Rocketdimensions = Rozmery rakety:
|
|||
|
|
pref.dlg.lbl.Linedensity = linie hustoty:
|
|||
|
|
pref.dlg.lbl.Motordimensions = Rozmery motoru:
|
|||
|
|
pref.dlg.lbl.Surfacedensity = Povrchov<EFBFBD> hustota:
|
|||
|
|
pref.dlg.lbl.Distance = Vzd<EFBFBD>lenost:
|
|||
|
|
pref.dlg.lbl.Bulkdensity = Objemov<EFBFBD> hustota:
|
|||
|
|
pref.dlg.lbl.Velocity = Rychlost:
|
|||
|
|
pref.dlg.lbl.Surfaceroughness = Hrubost povrchu:
|
|||
|
|
pref.dlg.lbl.Acceleration = Zrychlen<EFBFBD>:
|
|||
|
|
pref.dlg.lbl.Area = Oblast:
|
|||
|
|
pref.dlg.lbl.Mass = Hmostnost:
|
|||
|
|
pref.dlg.lbl.Angle = <EFBFBD>hel:
|
|||
|
|
pref.dlg.lbl.Force = S<EFBFBD>la:
|
|||
|
|
pref.dlg.lbl.Rollrate = M<EFBFBD>ra rotace:
|
|||
|
|
pref.dlg.lbl.Totalimpulse = Celkov<EFBFBD> impuls:
|
|||
|
|
pref.dlg.lbl.Temperature = Teplota:
|
|||
|
|
pref.dlg.lbl.Momentofinertia = Moment setrvacnosti:
|
|||
|
|
pref.dlg.lbl.Pressure = Tlak:
|
|||
|
|
pref.dlg.lbl.Stability = Stabilita:
|
|||
|
|
pref.dlg.lbl.FlightTime = Letov<EFBFBD> cas:
|
|||
|
|
pref.dlg.lbl.effect1 = Projev<EFBFBD> se pri dal\u0161<36>m otevren<65> okna.
|
|||
|
|
pref.dlg.lbl.Checkingupdates = Kontrola aktualizac<61>...
|
|||
|
|
pref.dlg.lbl.msg1 = Nastala chyba behem komunikace ze serverem.
|
|||
|
|
pref.dlg.lbl.msg2 = Nemohu z<>skat informace o aktualizac<61>ch
|
|||
|
|
pref.dlg.lbl.msg3 = Je spu\u0161tena nejnovej\u0161<36> verze programu OpenRocket.
|
|||
|
|
pref.dlg.lbl.msg4 = Nejsou dostupn<70> \u017E<37>dn<64> aktualizace
|
|||
|
|
pref.dlg.PrefChoiseSelector1 = Poka\u017Ed<45> se ptej
|
|||
|
|
pref.dlg.PrefChoiseSelector2 = Vlo\u017E doprostred
|
|||
|
|
pref.dlg.PrefChoiseSelector3 = Pridej na konec
|
|||
|
|
pref.dlg.PrefBooleanSelector1 = Sma\u017E
|
|||
|
|
pref.dlg.PrefBooleanSelector2 = Potvrd
|
|||
|
|
pref.dlg.Add = Pridej
|
|||
|
|
pref.dlg.DescriptionArea.Adddirectories = Pridej adres<65>re, soubory RASP motor (*.eng), RockSim engine soubory (*.rse) nebo ZIP archiv oddelen<65> oddelovacem (;) k nahr<68>n<EFBFBD> extern<72>ch v<>konov<6F>ch prubehu. Zmeny se projev<65> po restaru programu OpenRocket.
|
|||
|
|
|
|||
|
|
PreferencesDialog.lbl.language = Jazyk rohrann<6E>:
|
|||
|
|
PreferencesDialog.languages.default = V<EFBFBD>choz<EFBFBD>
|
|||
|
|
PreferencesDialog.lbl.languageEffect = Jazyk se zmen<65> pri dal\u0161<36>m spu\u0161ten<65> programu OpenRocket.
|
|||
|
|
|
|||
|
|
! Simulation edit dialog
|
|||
|
|
simedtdlg.but.runsimulation = Simulace be\u017E<37>
|
|||
|
|
simedtdlg.but.resettodefault = Reset do v<>choz<6F> hodnoty
|
|||
|
|
simedtdlg.but.add = Pridej
|
|||
|
|
simedtdlg.but.remove = Odeber
|
|||
|
|
simedtdlg.title.Editsim = Uprav simulaci
|
|||
|
|
simedtdlg.lbl.Simname = Jm<EFBFBD>no simulace:
|
|||
|
|
simedtdlg.tab.Launchcond = Startovac<EFBFBD> podm<64>nky
|
|||
|
|
simedtdlg.tab.Simopt = Parametry simulace
|
|||
|
|
simedtdlg.tab.Plotdata = Zobraz data
|
|||
|
|
simedtdlg.tab.Exportdata = Exportuj data
|
|||
|
|
simedtdlg.lbl.Motorcfg = Nastaven<EFBFBD> motoru:
|
|||
|
|
simedtdlg.lbl.ttip.Motorcfg = Nastav konfiguraci motoru k pouziti.
|
|||
|
|
simedtdlg.combo.ttip.motorconf = Nastav konfiguraci motoru k pouziti.
|
|||
|
|
simedtdlg.lbl.Wind = V<EFBFBD>tr
|
|||
|
|
simedtdlg.lbl.Averwindspeed = Prumern<EFBFBD> rychlost vetru:
|
|||
|
|
simedtdlg.lbl.ttip.Averwindspeed = Prumern<EFBFBD> rychlost vetru vzhledem k zemi.
|
|||
|
|
simedtdlg.lbl.Stddeviation = Standartn<EFBFBD> odchylka:
|
|||
|
|
simedtdlg.lbl.ttip.Stddeviation = <html>Standartn<74> odchylka rychlosti vetru.<br>Rychlost vetru je v r<>mci dvojn<6A>sobku standartn<74> odchylky od prumeru po 95% casu.
|
|||
|
|
simedtdlg.lbl.Turbulenceintensity = Intenzita turbulenc<6E>:
|
|||
|
|
simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>Intenzita turbulenc<6E> je standartn<74> odchylka delen<65> prumerem rychlosti vetru.<br>
|
|||
|
|
simedtdlg.lbl.ttip.Turbulenceintensity2 = Typick<EFBFBD> hodnoty od
|
|||
|
|
simedtdlg.lbl.ttip.Turbulenceintensity3 = do
|
|||
|
|
simedtdlg.border.Atmoscond = Atmosf<EFBFBD>rick<EFBFBD> podm<64>nky
|
|||
|
|
simedtdlg.checkbox.InterStdAtmosphere = Pou\u017Eij mezin<69>rodn<64> standardizovanou atmosf<73>ru
|
|||
|
|
simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Oznac k pou\u017Eit<69> mezin<69>rodn<64> model standartn<74> atmodf<64>ry.<br>Tento model m<> teplotu
|
|||
|
|
simedtdlg.checkbox.ttip.InterStdAtmosphere2 = a tlak
|
|||
|
|
simedtdlg.checkbox.ttip.InterStdAtmosphere3 = na <20>rovni mors<72> hladiny.
|
|||
|
|
simedtdlg.lbl.Temperature = Teplota:
|
|||
|
|
simedtdlg.lbl.ttip.Temperature = Teplota na startovn<76> plo\u0161e.
|
|||
|
|
simedtdlg.lbl.Pressure = Tlak:
|
|||
|
|
simedtdlg.lbl.ttip.Pressure = Atmosf<EFBFBD>rick<EFBFBD> tlak na startovn<76> plo\u0161e.
|
|||
|
|
simedtdlg.lbl.Launchsite = M<EFBFBD>sto startu
|
|||
|
|
simedtdlg.lbl.Latitude = Zemepisn<EFBFBD> \u0161<36>rka:
|
|||
|
|
simedtdlg.lbl.ttip.Latitude = <html>Zemepisn<73> \u0161<36>rka ovlivnuje gravitacn<63> s<>lu zeme.<br>Pozitivn<76> hodnoty jsou na Severn<72> polokouli, negativn<76> na ji\u017En<45> polokouli.
|
|||
|
|
|
|||
|
|
simedtdlg.lbl.Longitude = Zemepisn<EFBFBD> d<>lka:
|
|||
|
|
simedtdlg.lbl.ttip.Longitude = <html>Vy\u017Eadov<6F>no pro predpoved pocas<61> a letov<6F> model.
|
|||
|
|
|
|||
|
|
simedtdlg.lbl.Altitude = Nadmorsk<EFBFBD> v<>\u0161ka:
|
|||
|
|
simedtdlg.lbl.ttip.Altitude = <html>Startovn<76> nadmorsk<73> v<>\u0161ka na <20>rovni hladiny more.<br>Toto ovlivnuje pozici rakety v atmosf<73>rick<63>m modelu.
|
|||
|
|
simedtdlg.border.Launchrod = Startovn<EFBFBD> pozice
|
|||
|
|
simedtdlg.lbl.Length = D<EFBFBD>lka:
|
|||
|
|
simedtdlg.lbl.ttip.Length = D<EFBFBD>lka startovn<76> pozice.
|
|||
|
|
simedtdlg.lbl.Angle = <EFBFBD>hel:
|
|||
|
|
simedtdlg.lbl.ttip.Angle = <EFBFBD>hel startovn<76> pozice od vertik<69>ly.
|
|||
|
|
simedtdlg.lbl.Direction = Smer:
|
|||
|
|
simedtdlg.lbl.ttip.Direction1 = <html>Smer vypu\u0161ten<65> vzhledem k vetru.<br>
|
|||
|
|
simedtdlg.lbl.ttip.Direction2 = = Proti vetru,
|
|||
|
|
simedtdlg.lbl.ttip.Direction3 = = po vetru.
|
|||
|
|
simedtdlg.border.Simopt = Vlastnosti simul<75>toru
|
|||
|
|
simedtdlg.lbl.Calcmethod = V<EFBFBD>pocetn<EFBFBD> metoda:
|
|||
|
|
simedtdlg.lbl.ttip.Calcmethod = <html>Roz\u0161<36>ren<65> Barrowmanova metoda poc<6F>t<EFBFBD> aerodynamick<63> s<>ly vzhledem <br>to Roz\u0161<36>ren<65> Barrowmanovi rovnice pojmou v<>ce podm<64>nek.
|
|||
|
|
simedtdlg.lbl.ExtBarrowman = Roz\u0161<36>ren<65> Barrowman
|
|||
|
|
simedtdlg.lbl.Simmethod = Simulacn<EFBFBD> metoda:
|
|||
|
|
simedtdlg.lbl.ttip.Simmethod1 = <html>\u0160est stupnu volnosti simul<75>toru umo\u017Enuje rakete celkovou svobodu behem letu.<br>
|
|||
|
|
simedtdlg.lbl.ttip.Simmethod2 = Integrace je poc<6F>t<EFBFBD>na za pomoci 4<sup>th</sup> stupnov<6F> Runge-Kuttoovi numerick<63> integrace.
|
|||
|
|
simedtdlg.lbl.GeodeticMethod = Geodetick<EFBFBD> v<>pocty:
|
|||
|
|
simedtdlg.lbl.ttip.GeodeticMethodTip = Pripraven vypoc<6F>tat povrchov<6F> koordin<69>ty. TO tak<61> aktivuje v<>pocet koriolisovy s<>ly.
|
|||
|
|
simedtdlg.lbl.Timestep = Casov<EFBFBD> krok:
|
|||
|
|
simedtdlg.lbl.ttip.Timestep1 = <html>Cas mezi simulacn<63>mi kroky.<br>Men\u0161<36> dobu kroku znamen<65> pomalej\u0161<36> v<>pocet, ale vy\u0161\u0161<36> presnost v<>poctu.<br>
|
|||
|
|
simedtdlg.lbl.ttip.Timestep2 = Ctyr stupnov<6F> simulace je pomerne presn<73> s d<>lkou kroku
|
|||
|
|
simedtdlg.but.ttip.resettodefault = Resetuj d<>lku kroku na tuto v<>choz<6F> hodnotu (
|
|||
|
|
simedtdlg.border.Simlist = Dal\u0161<36> zpracov<6F>n<EFBFBD> simulace
|
|||
|
|
simedtdlg.txt.longA1 = <html><i>Dal\u0161<36> zpacov<6F>n<EFBFBD> simulace</i> je pokrocil<69> technika, kter<65> dovoluje pou\u017E<37>t u\u017Eivatelsk<73> k<>d k zpracov<6F>n<EFBFBD> dat ze simulace a k interakci ze simulac<61>.
|
|||
|
|
simedtdlg.txt.longA2 = Pro detailn<6C> popis jak ps<70>t skripty na dal\u0161<36> zpracov<6F>n<EFBFBD> simulace otevrete technickou dokumentaci k programu OpenRocket.
|
|||
|
|
simedtdlg.lbl.Curlist = Aktivn<EFBFBD> skript na dal\u0161<36> zpracov<6F>n<EFBFBD> simulace:
|
|||
|
|
simedtdlg.lbl.Addsimlist = Pridej skript na dal\u0161<36> zpracov<6F>n<EFBFBD> simulace
|
|||
|
|
simedtdlg.lbl.Noflightdata = Nejsou dostupn<70> letov<6F> data.
|
|||
|
|
simedtdlg.lbl.runsimfirst = Pros<EFBFBD>m jako prvn<76> spustte simulaci.
|
|||
|
|
simedtdlg.chart.Simflight = Letov<EFBFBD> simulace
|
|||
|
|
simedtdlg.dlg.Simres = V<EFBFBD>sledky simulace
|
|||
|
|
simedtdlg.IntensityDesc.None = \u017D<37>dn<64>
|
|||
|
|
simedtdlg.IntensityDesc.Verylow = Velmi n<>zk<7A>
|
|||
|
|
simedtdlg.IntensityDesc.Low = N<EFBFBD>zk<EFBFBD>
|
|||
|
|
simedtdlg.IntensityDesc.Medium = Stredn<EFBFBD>
|
|||
|
|
simedtdlg.IntensityDesc.High = Velk<EFBFBD>
|
|||
|
|
simedtdlg.IntensityDesc.Veryhigh = Velmi velk<6C>
|
|||
|
|
simedtdlg.IntensityDesc.Extreme = Extr<EFBFBD>mn<EFBFBD>
|
|||
|
|
|
|||
|
|
GeodeticComputationStrategy.flat.name = Rovn<EFBFBD> Zeme
|
|||
|
|
GeodeticComputationStrategy.flat.desc = Vykonej v<>pocet s aproximac<61> ploch<63> Zeme. Ten je dostatecnou presnost pro n<>zkov<6F>\u0161kov<6F> lety.
|
|||
|
|
GeodeticComputationStrategy.spherical.name = Sf<EFBFBD>rick<EFBFBD> aproximace
|
|||
|
|
GeodeticComputationStrategy.spherical.desc = <html>Vykonej geodetick<63> v<>pocet predpokl<6B>daj<61>c<EFBFBD> kulovou Zemi.<br>Ten m<> dostatecnou presnost pro v\u0161echny <20>cely.
|
|||
|
|
GeodeticComputationStrategy.wgs84.name = WGS84 ellipsa
|
|||
|
|
GeodeticComputationStrategy.wgs84.desc = <html>Proved geodetick<63> v<>pocet na WGS84 elipse za pou\u017Eit<69> Vincentovy metody.<br>Pomal<61> a nedostatecn<63> ve vet\u0161ine pr<70>padu.
|
|||
|
|
|
|||
|
|
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Simulation Panel
|
|||
|
|
simpanel.but.newsimulation = Nov<EFBFBD> simulace
|
|||
|
|
simpanel.but.editsimulation = Edituj simulaci
|
|||
|
|
simpanel.but.runsimulations = Spust simulaci
|
|||
|
|
simpanel.but.deletesimulations = Sma\u017E simulaci
|
|||
|
|
simpanel.but.plotexport = Vykresli / exportuj
|
|||
|
|
simpanel.but.ttip.newsimulation = Pridej novou simulaci
|
|||
|
|
simpanel.but.ttip.editsim = Edituj oznacenou simulaci
|
|||
|
|
simpanel.but.ttip.runsimu = Znovu spust oznacenou simulaci
|
|||
|
|
simpanel.but.ttip.deletesim = Sma\u017E oznacenou simulaci
|
|||
|
|
simpanel.checkbox.donotask = Neptejte se me znovu
|
|||
|
|
simpanel.lbl.defpref = Mu\u017Eete zmenit v<>choz<6F> cinost v nastaven<65>.
|
|||
|
|
simpanel.dlg.lbl.DeleteSim1 = Smazat oznacenou simulaci?
|
|||
|
|
simpanel.dlg.lbl.DeleteSim2 = <html><i>Tato operace nemu\u017Ee b<>t vzata zpet.</i>
|
|||
|
|
simpanel.dlg.lbl.DeleteSim3 = Sma\u017E simulaci
|
|||
|
|
simpanel.col.Name = Jm<EFBFBD>no
|
|||
|
|
simpanel.col.Motors = Motory
|
|||
|
|
simpanel.col.Velocityoffrod = Rychlost ot<6F>cen<65>
|
|||
|
|
simpanel.col.Velocityatdeploy = Rychlost v nasazen<65>
|
|||
|
|
simpanel.col.Apogee = Vrchol
|
|||
|
|
simpanel.col.Maxvelocity = Max. rychlost
|
|||
|
|
simpanel.col.Maxacceleration = Max. zrychlen<65>
|
|||
|
|
simpanel.col.Timetoapogee = Cas do dosa\u017Een<65> vrcholu
|
|||
|
|
simpanel.col.Flighttime = Letov<EFBFBD> cas
|
|||
|
|
simpanel.col.Groundhitvelocity = Rychlost pri dopadu na zem
|
|||
|
|
|
|||
|
|
! SimulationRunDialog
|
|||
|
|
SimuRunDlg.title.RunSim = Simulace be\u017E<37>...
|
|||
|
|
SimuRunDlg.lbl.Running = Be\u017E<37> ...
|
|||
|
|
SimuRunDlg.lbl.Simutime = Doba simulace:
|
|||
|
|
SimuRunDlg.lbl.Altitude = V<EFBFBD>\u0161ka:
|
|||
|
|
SimuRunDlg.lbl.Velocity = Rychlost:
|
|||
|
|
SimuRunDlg.msg.Unabletosim = Nemo\u017Enost simulovat:
|
|||
|
|
SimuRunDlg.msg.errorOccurred = Chyba nastala behem simulace:
|
|||
|
|
SimuRunDlg.msg.AnException1 = Vyj<EFBFBD>mka nastala behem simulace:
|
|||
|
|
SimuRunDlg.msg.AnException2 = Pros<EFBFBD>m oznamte toto jako chybu z<>roven s detaily n<>\u017Ee.
|
|||
|
|
SimuRunDlg.msg.AssertionError1 = Chyba ve v<>poctu nastala behem simulace.
|
|||
|
|
SimuRunDlg.msg.AssertionError2 = Pros<EFBFBD>m oznamte toto jako chybu z<>roven s detaily n<>\u017Ee.
|
|||
|
|
SimuRunDlg.msg.unknownerror1 = Nezn<EFBFBD>m<EFBFBD> chyba se vyskytla behem simulace.
|
|||
|
|
SimuRunDlg.msg.unknownerror2 = Program mu\u017Ee b<>t nestabiln<6C> mel by-jste ulo\u017Eit v\u0161echny va\u0161e n<>vrhy a okam\u017Eite restartovat OpenRocket !
|
|||
|
|
|
|||
|
|
|
|||
|
|
RK4SimulationStepper.error.valuesTooLarge = Hodnoty simulace prekrocily limity. Zkuste nastavit krat\u0161<36> d<>lku kroku.
|
|||
|
|
|
|||
|
|
|
|||
|
|
! SimulationExportPanel
|
|||
|
|
SimExpPan.desc = Soubory s c<>rkov<6F>m oddelovacem (*.csv)
|
|||
|
|
SimExpPan.border.Vartoexport = Promenn<EFBFBD> k exportu
|
|||
|
|
SimExpPan.but.Selectall = Oznac v\u0161e
|
|||
|
|
SimExpPan.but.Selectnone = Nic neoznacuj
|
|||
|
|
SimExpPan.border.Fieldsep = Oddelovac prvku
|
|||
|
|
SimExpPan.lbl.Fieldsepstr = Retezec slou\u017E<37>c<EFBFBD> k oddelov<6F>n<EFBFBD> prvku:
|
|||
|
|
SimExpPan.lbl.longA1 = <html>Retezec slou\u017E<37>c<EFBFBD> k oddelen<65> prvku v exportovan<61>m souboru.<br>
|
|||
|
|
SimExpPan.lbl.longA2 = Pou\u017Eij ',' pro soubory s hodnotami oddelen<65>mi carkou (CSV) soubor.
|
|||
|
|
SimExpPan.checkbox.Includesimudesc = Vlo\u017E popis simulace
|
|||
|
|
SimExpPan.checkbox.ttip.Includesimudesc = Vlo\u017E koment<6E>r na zac<61>tek souboru popisuj<75>c<EFBFBD>ho simulaci.
|
|||
|
|
SimExpPan.border.Comments = Koment<EFBFBD>re
|
|||
|
|
SimExpPan.checkbox.Includefielddesc = Obsahuje popis prvku
|
|||
|
|
SimExpPan.checkbox.ttip.Includefielddesc = Obsahuje koment<6E>r s popisem exportovan<61>ch hodnot.
|
|||
|
|
SimExpPan.checkbox.Incflightevents = Obsahuje letov<6F> ud<75>losti
|
|||
|
|
SimExpPan.checkbox.ttip.Incflightevents = Obsahuje koment<6E>r pro ka\u017Ed<45> letov<6F> parametr.
|
|||
|
|
SimExpPan.lbl.Commentchar = Uvozuj<EFBFBD>c<EFBFBD> retezec koment<6E>re:
|
|||
|
|
SimExpPan.lbl.ttip.Commentchar = Tyto znaky oznacuj<75> koment<6E>r.
|
|||
|
|
SimExpPan.but.Exporttofile = Exportuj do souboru...
|
|||
|
|
SimExpPan.Fileexists.desc1 = Soubor \"
|
|||
|
|
SimExpPan.Fileexists.desc2 = \" existuje. Chcete ho prepsat?
|
|||
|
|
SimExpPan.Fileexists.title = Soubor existuje
|
|||
|
|
SimExpPan.ExportingVar.desc1 = Exportuji 1 promennou od
|
|||
|
|
SimExpPan.ExportingVar.desc2 = Exportuji
|
|||
|
|
SimExpPan.ExportingVar.desc3 = promenn<EFBFBD> od
|
|||
|
|
SimExpPan.Col.Variable = Promenn<EFBFBD>
|
|||
|
|
SimExpPan.Col.Unit = Jednoty
|
|||
|
|
|
|||
|
|
|
|||
|
|
CsvOptionPanel.separator.space = Mezern<EFBFBD>k
|
|||
|
|
CsvOptionPanel.separator.tab = Tabul<EFBFBD>tor
|
|||
|
|
|
|||
|
|
|
|||
|
|
|
|||
|
|
! MotorPlot
|
|||
|
|
MotorPlot.title.Motorplot = Graf motoru
|
|||
|
|
MotorPlot.but.Select = Vyber
|
|||
|
|
MotorPlot.Chart.Motorthrustcurve = V<EFBFBD>konov<EFBFBD> krivka motoru
|
|||
|
|
MotorPlot.Chart.Time = Cas / s
|
|||
|
|
MotorPlot.Chart.Thrust = V<EFBFBD>kon / N
|
|||
|
|
MotorPlot.txt.Designation = Oznacen<EFBFBD>:
|
|||
|
|
MotorPlot.txt.Manufacturer = V<EFBFBD>robce:
|
|||
|
|
MotorPlot.txt.Type = Typ:
|
|||
|
|
MotorPlot.txt.Delays = Zpo\u017Een<65>:
|
|||
|
|
MotorPlot.txt.Comment = Koment<EFBFBD>r:\n
|
|||
|
|
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Simulation plot panel
|
|||
|
|
simplotpanel.lbl.Presetplotconf = Prednastaven<EFBFBD> parametry vykreslen<65> grafu:
|
|||
|
|
simplotpanel.lbl.Xaxistype = Typ osy X:
|
|||
|
|
simplotpanel.lbl.Unit = Jednotky:
|
|||
|
|
simplotpanel.lbl.Yaxistypes = Typ osy Y:
|
|||
|
|
simplotpanel.lbl.Flightevents = Letov<EFBFBD> ud<75>losti:
|
|||
|
|
simplotpanel.but.All = V\u0161e
|
|||
|
|
simplotpanel.but.None = Nic
|
|||
|
|
simplotpanel.but.NewYaxisplottype = Nov<EFBFBD> typ osy Y
|
|||
|
|
simplotpanel.but.Plotflight = Letov<EFBFBD> graf
|
|||
|
|
simplotpanel.lbl.Axis = Osy:
|
|||
|
|
simplotpanel.but.ttip.Removethisplot = Odeber tento graf
|
|||
|
|
simplotpanel.Desc = Data budou vykreslena v casov<6F>m porad<61> i kdy\u017E osa x nebude nastavena jako cas.
|
|||
|
|
simplotpanel.OptionPane.lbl1 = Maxim<EFBFBD>lne 15 grafu je povoleno.
|
|||
|
|
simplotpanel.OptionPane.lbl2 = Nemohu pridat graf
|
|||
|
|
simplotpanel.AUTO_NAME = Automaticky
|
|||
|
|
simplotpanel.LEFT_NAME = Vlevo
|
|||
|
|
simplotpanel.RIGHT_NAME = Vpravo
|
|||
|
|
simplotpanel.CUSTOM = Vlastn<EFBFBD>
|
|||
|
|
SimulationPlotPanel.error.noPlotSelected = Pros<EFBFBD>m pridejte jednu nebo v<>ce promen<65>ch v grafu na osu Y.
|
|||
|
|
SimulationPlotPanel.error.noPlotSelected.title = Nic k vykreslen<65>
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Component add buttons
|
|||
|
|
compaddbuttons.Bodycompandfinsets = Komponenty tela a stabiliz<69>tory
|
|||
|
|
compaddbuttons.Nosecone = Pr<EFBFBD>dov<EFBFBD> ku\u017Eel
|
|||
|
|
compaddbuttons.Bodytube = Trubka tela
|
|||
|
|
compaddbuttons.Transition = Prechod trupu
|
|||
|
|
compaddbuttons.Trapezoidal = Trap<EFBFBD>zoidn<EFBFBD>
|
|||
|
|
compaddbuttons.Elliptical = Eliptyck<EFBFBD>
|
|||
|
|
compaddbuttons.Freeform = Voln<EFBFBD> tvar
|
|||
|
|
compaddbuttons.Launchlug = Vypou\u0161tec<65> oko
|
|||
|
|
compaddbuttons.Innercomponent = Vnitrn<EFBFBD> komponenty
|
|||
|
|
compaddbuttons.Innertube = Vnitrn<EFBFBD> trubka
|
|||
|
|
compaddbuttons.Coupler = Pr<EFBFBD>pojka
|
|||
|
|
compaddbuttons.Centeringring = Stred\nring
|
|||
|
|
compaddbuttons.Bulkhead = Prep<EFBFBD>\u017Eka
|
|||
|
|
compaddbuttons.Engineblock = Motor\nblock
|
|||
|
|
compaddbuttons.Massobjects = Z<EFBFBD>va\u017E<37>
|
|||
|
|
compaddbuttons.Parachute = Pad<EFBFBD>k
|
|||
|
|
compaddbuttons.Streamer = Stuha
|
|||
|
|
compaddbuttons.Shockcord = Poutac<EFBFBD> \u0161nura
|
|||
|
|
compaddbuttons.Masscomponent = Hmotnost\ncomponent
|
|||
|
|
compaddbuttons.Donotaskmeagain = Neptejte me me znovu
|
|||
|
|
compaddbuttons.Selectcomppos = Oznac pozici komponenty
|
|||
|
|
compaddbuttons.lbl.Youcanchange = Mu\u017Eete zmenit v<>choz<6F> operace v z<>lo\u017Ece mo\u017Enosti.
|
|||
|
|
compaddbuttons.lbl.insertcomp = Vlo\u017Eit komponentu za soucasnou nebo posledn<64> komponentu ?
|
|||
|
|
compaddbuttons.askPosition.Inserthere = Vlo\u017E zde
|
|||
|
|
compaddbuttons.askPosition.Addtotheend = Pridej na konec
|
|||
|
|
compaddbuttons.askPosition.Cancel = Zru\u0161it
|
|||
|
|
|
|||
|
|
! Component Analysis Dialog
|
|||
|
|
componentanalysisdlg.componentanalysis = Anal<EFBFBD>za souc<75>stky
|
|||
|
|
componentanalysisdlg.lbl.winddir = Smer vetru:
|
|||
|
|
componentanalysisdlg.TitledBorder.warnings = Varov<EFBFBD>n<EFBFBD>:
|
|||
|
|
componentanalysisdlg.ToggleBut.worst = Nejhor\u0161<36>
|
|||
|
|
componentanalysisdlg.lbl.angleofattack = <EFBFBD>hel n<>behu:
|
|||
|
|
componentanalysisdlg.lbl.machnumber = Machovo c<>slo:
|
|||
|
|
componentanalysisdlg.lbl.rollrate = Rychlost ot<6F>cen<65>:
|
|||
|
|
componentanalysisdlg.lbl.activestages = Startovac<EFBFBD> rampa:
|
|||
|
|
componentanalysisdlg.lbl.motorconf = Nastaven<EFBFBD> motoru:
|
|||
|
|
componentanalysisdlg.TabStability.Col = Komponenta
|
|||
|
|
componentanalysisdlg.TabStability = Stabilita
|
|||
|
|
componentanalysisdlg.TabStability.ttip = Informace o stabilite
|
|||
|
|
componentanalysisdlg.dragTableModel.Col.Component = Komponenta
|
|||
|
|
componentanalysisdlg.dragTableModel.Col.Pressure = <html>Tlak C<sub>D</sub>
|
|||
|
|
componentanalysisdlg.dragTableModel.Col.Base = <html>Z<>kladn<64> C<sub>D</sub>
|
|||
|
|
componentanalysisdlg.dragTableModel.Col.friction = <html>Tren<65> C<sub>D</sub>
|
|||
|
|
componentanalysisdlg.dragTableModel.Col.total = <html>Celkem C<sub>D</sub>
|
|||
|
|
componentanalysisdlg.dragTabchar = Vlastnosti trupu
|
|||
|
|
componentanalysisdlg.dragTabchar.ttip = Drag characteristics
|
|||
|
|
componentanalysisdlg.rollTableModel.Col.component = Komponenta
|
|||
|
|
componentanalysisdlg.rollTableModel.Col.rollforc = Ot<EFBFBD>cec<EFBFBD> koefficient
|
|||
|
|
componentanalysisdlg.rollTableModel.Col.rolldamp = Ot<EFBFBD>cec<EFBFBD> tlum<75>c<EFBFBD> coefficient
|
|||
|
|
componentanalysisdlg.rollTableModel.Col.total = <html>Celkem C<sub>l</sub>
|
|||
|
|
componentanalysisdlg.rollTableModel = Ot<EFBFBD>cec<EFBFBD> dynamika
|
|||
|
|
componentanalysisdlg.rollTableModel.ttip = Ot<EFBFBD>cec<EFBFBD> dynamika
|
|||
|
|
componentanalysisdlg.println.closingmethod = Jm<EFBFBD>no uzav<61>rac<61> metody:
|
|||
|
|
componentanalysisdlg.println.settingnam = Nastaven<EFBFBD> NAN hodnot
|
|||
|
|
componentanalysisdlg.lbl.reflenght = Doporucen<EFBFBD> d<>lka:
|
|||
|
|
componentanalysisdlg.lbl.refarea = Doporucen<EFBFBD> plocha:
|
|||
|
|
!componentanalysisdlg.But.close = Zavr<76>t
|
|||
|
|
componentanalysisdlg.TabStability.Col.Component = Komponenta
|
|||
|
|
|
|||
|
|
! Custom Material dialog
|
|||
|
|
custmatdlg.title.Custommaterial = Vlastn<EFBFBD> materi<72>l
|
|||
|
|
custmatdlg.lbl.Materialname = Jm<EFBFBD>no materi<72>lu:
|
|||
|
|
custmatdlg.lbl.Materialtype = Typ materi<72>lu:
|
|||
|
|
custmatdlg.lbl.Materialdensity = Hustota materi<72>lu:
|
|||
|
|
custmatdlg.checkbox.Addmaterial = Pridej materi<72>l do datab<61>ze
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Ring Component Config
|
|||
|
|
ringcompcfg.OuterRadius = Vnej\u0161<36> r<>dius
|
|||
|
|
ringcompcfg.Automatic = Automaticky
|
|||
|
|
ringcompcfg.InnerRadius = Vnitrn<EFBFBD> r<>dius
|
|||
|
|
ringcompcfg.Thickness = Tloustka
|
|||
|
|
ringcompcfg.Length = D<EFBFBD>lka
|
|||
|
|
ringcompcfg.Positionrelativeto = Pozice vzhledem k:
|
|||
|
|
ringcompcfg.plus = plus
|
|||
|
|
ringcompcfg.PositionValue = Hodnota pozice
|
|||
|
|
ringcompcfg.Radialdistance = Radi<EFBFBD>ln<EFBFBD> vzd<7A>lenost:
|
|||
|
|
ringcompcfg.Distancefrom = Vzd<EFBFBD>lenost od osy rakety
|
|||
|
|
ringcompcfg.Radialdirection = Radi<EFBFBD>ln<EFBFBD> smer:
|
|||
|
|
ringcompcfg.radialdirectionfrom = Radi<EFBFBD>ln<EFBFBD> vzd<7A>lenost od smeru osy
|
|||
|
|
ringcompcfg.but.Reset = Reset
|
|||
|
|
ringcompcfg.but.Resetcomponant = Resetuj komponentu od osy rakety
|
|||
|
|
ringcompcfg.EngineBlock.desc = <html>An <b>blok motoru</b> zastav<61> motor v pohybu vzad v motorov<6F> trubici.<br><br>Pokud se prid<69> motor vytvor<6F> <b>telo</b> nebo <b>skrytou trubku tube</b> a oznac<61> ji jako mont<6E>\u017E motoru v<em>Motoru</em> tab.
|
|||
|
|
ringcompcfg.note.desc = Pozn<EFBFBD>mka: Vnitrn<72> trubka nem<65> effekt na aerodynamiku motoru i kdy\u017E je um<75>stena mimo telo rakety.
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Body Tube Config
|
|||
|
|
BodyTubecfg.lbl.Bodytubelength = D<EFBFBD>lka tela rakety:
|
|||
|
|
BodyTubecfg.lbl.Outerdiameter = Vnej\u0161<36> prumer:
|
|||
|
|
BodyTubecfg.lbl.Innerdiameter = Vnitrn<EFBFBD> prumer:
|
|||
|
|
BodyTubecfg.lbl.Wallthickness = Tlou\u0161tka steny:
|
|||
|
|
BodyTubecfg.tab.General = Obecne
|
|||
|
|
BodyTubecfg.tab.Generalproperties = Obecn<EFBFBD> vlastnosti
|
|||
|
|
BodyTubecfg.tab.Motor = Motor
|
|||
|
|
BodyTubecfg.tab.Motormountconf = Konfigurace pripojen<65> motoru
|
|||
|
|
BodyTubecfg.checkbox.Automatic = Automaticky
|
|||
|
|
BodyTubecfg.checkbox.Filled = Vyplnen<EFBFBD>
|
|||
|
|
|
|||
|
|
! FinSetConfig
|
|||
|
|
FinSetConfig.tab.Fintabs = Stabiliz<EFBFBD>tory
|
|||
|
|
FinSetConfig.tab.Through-the-wall = \u017Dlab mezi stenou a stabiliz<69>tory
|
|||
|
|
FinSetConfig.but.Converttofreeform = Konvertovat na voln<6C> tvar
|
|||
|
|
FinSetConfig.but.Converttofreeform.ttip = Konvertuj tyto stabiliz<69>tory na volno tvarov<6F> stabiliz<69>tory
|
|||
|
|
FinSetConfig.Convertfinset = Konvertuj stabiliz<69>tory
|
|||
|
|
FinSetConfig.but.Splitfins = Rozdel stabiliz<69>tory
|
|||
|
|
FinSetConfig.but.Splitfins.ttip = Rozdel stabili<6C>tory na samostatn<74>
|
|||
|
|
FinSetConfig.but.AutoCalc = Vypocti automaticky
|
|||
|
|
FinSetConfig.lbl.Through-the-wall = \u017Dlab mezi stenou a stabiliz<69>tory:
|
|||
|
|
FinSetConfig.lbl.Tablength = D<EFBFBD>lka stabiliz<69>toru:
|
|||
|
|
FinSetConfig.ttip.Tablength = Delka stabiliz<69>toru.
|
|||
|
|
FinSetConfig.lbl.Tabheight = \u0160<36>rka stabiliz<69>toru:
|
|||
|
|
FinSetConfig.ttip.Tabheight = \u0160<36>rka rozpet<65> mezi stabiliz<69>tory.
|
|||
|
|
FinSetConfig.lbl.Tabposition = Pozice stabiliz<69>toru:
|
|||
|
|
FinSetConfig.ttip.Tabposition = Pozice stabiliz<69>toru.
|
|||
|
|
FinSetConfig.lbl.relativeto = Vzhledem k
|
|||
|
|
|
|||
|
|
!FinMarkingGuide
|
|||
|
|
FinMarkingGuide.lbl.Front = Predn<EFBFBD> strana
|
|||
|
|
|
|||
|
|
! MotorDatabaseLoadingDialog
|
|||
|
|
MotorDbLoadDlg.title = Plnen<EFBFBD> motoru
|
|||
|
|
MotorDbLoadDlg.Loadingmotors = Plnen<EFBFBD> motoru...
|
|||
|
|
|
|||
|
|
! RocketConfig
|
|||
|
|
RocketCfg.lbl.Designname = Jm<EFBFBD>no n<>vrhu:
|
|||
|
|
RocketCfg.lbl.Designer = N<EFBFBD>vrh<EFBFBD>r:
|
|||
|
|
RocketCfg.lbl.Comments = Koment<EFBFBD>re:
|
|||
|
|
RocketCfg.lbl.Revisionhistory = Prehled historie:
|
|||
|
|
RocketCfg.lbl.Material = Materi<EFBFBD>l:
|
|||
|
|
|
|||
|
|
! ShockCordConfig
|
|||
|
|
ShockCordCfg.lbl.Shockcordlength = D<EFBFBD>lka poutac<61> \u0161nury:
|
|||
|
|
|
|||
|
|
! RocketComponentConfig
|
|||
|
|
RocketCompCfg.lbl.Componentname = Jm<EFBFBD>no komponenty:
|
|||
|
|
RocketCompCfg.ttip.Thecomponentname = Jm<EFBFBD>no komponenty.
|
|||
|
|
RocketCompCfg.tab.Override = Prepsat
|
|||
|
|
RocketCompCfg.tab.MassandCGoverride = Prepi\u0161 hmotnost a te\u017Ei\u0161te
|
|||
|
|
RocketCompCfg.tab.Figure = Obr<EFBFBD>zek
|
|||
|
|
RocketCompCfg.tab.Figstyleopt = Vlastnosti obr<62>zku
|
|||
|
|
RocketCompCfg.tab.Comment = Koment<EFBFBD>r
|
|||
|
|
RocketCompCfg.tab.Specifyacomment = Upresnen<EFBFBD> koment<6E>re komponenty
|
|||
|
|
RocketCompCfg.lbl.Mass = Hmotnost:
|
|||
|
|
RocketCompCfg.lbl.Componentmass = Hmotnost komponenty:
|
|||
|
|
RocketCompCfg.lbl.overriddento = (preps<70>no na
|
|||
|
|
RocketCompCfg.lbl.overriddenby = (preps<70>no
|
|||
|
|
RocketCompCfg.lbl.Componentmaterial = Materi<EFBFBD>l komponentu:
|
|||
|
|
RocketCompCfg.lbl.Componentfinish = Povrchov<EFBFBD> <20>prava komponenty:
|
|||
|
|
RocketCompCfg.lbl.ttip.componentmaterialaffects = Materi<EFBFBD>l komponenty ovlivnuje v<>hu komponety.
|
|||
|
|
RocketCompCfg.combo.ttip.componentmaterialaffects = Materi<EFBFBD>l komponenty ovlivnuje v<>hu komponety.
|
|||
|
|
RocketCompCfg.lbl.longA1 = <html> Povrchov<6F> <20>prava komponenty ovlivnuje aerodynamiku komponenty.<br>
|
|||
|
|
RocketCompCfg.lbl.longA2 = Hodnota odpov<6F>d<EFBFBD> prumern<72> hrubosti povrchu.
|
|||
|
|
RocketCompCfg.but.Setforall = Nastav pro v\u0161echny
|
|||
|
|
RocketCompCfg.but.ttip.Setforall = Nastav povrchovou <20>pravu pro v\u0161echny komponenty rakety.
|
|||
|
|
RocketCompCfg.lbl.Overridemassorcenter = Zmen hmotnost nebo te\u017Ei\u0161te
|
|||
|
|
RocketCompCfg.checkbox.Overridemass = Zmen hmotnost:
|
|||
|
|
RocketCompCfg.checkbox.Overridecenterofgrav = Zmen te\u017Ei\u0161te:
|
|||
|
|
RocketCompCfg.checkbox.OverridemassandCG = Zmen hmotnost a te\u017Ei\u0161te v\u0161ech komponent
|
|||
|
|
RocketCompCfg.lbl.longB1 = <html> Zmena hmotnosti nezahrnuje motory.<br>
|
|||
|
|
RocketCompCfg.lbl.longB2 = Te\u017Ei\u0161te je mereno od predku
|
|||
|
|
RocketCompCfg.lbl.Commentsonthe = Koment<EFBFBD>r na
|
|||
|
|
RocketCompCfg.lbl.Figurestyle = Styl obr<62>tku:
|
|||
|
|
RocketCompCfg.lbl.Componentcolor = Barva komponenty:
|
|||
|
|
RocketCompCfg.lbl.Choosecolor = Vyber barvu
|
|||
|
|
RocketCompCfg.checkbox.Usedefaultcolor = Pou\u017Eij v<>choz<6F> barvu
|
|||
|
|
RocketCompCfg.lbl.Complinestyle = Styl c<>ry:
|
|||
|
|
RocketCompCfg.but.Saveasdefstyle = Ulo\u017E jako v<>choz<6F> styl
|
|||
|
|
RocketCompCfg.lbl.Diameter = Prumer:
|
|||
|
|
RocketCompCfg.lbl.Length = D<EFBFBD>lka:
|
|||
|
|
RocketCompCfg.lbl.Thickness = Tlou\u0161tka:
|
|||
|
|
RocketCompCfg.checkbox.Endcapped = Z<EFBFBD>slepka
|
|||
|
|
RocketCompCfg.ttip.Endcapped = Zdali je konec ramene zaslepen.
|
|||
|
|
RocketCompCfg.title.Noseconeshoulder = Dr\u017E<37>k nosn<73>ho d<>lu
|
|||
|
|
RocketCompCfg.title.Aftshoulder = Dr\u017E<37>k z<>di
|
|||
|
|
RocketCompCfg.border.Foreshoulder = Dr\u017E<37>k pr<70>di
|
|||
|
|
!RocketCompCfg.lbl.Length = D<>lka:
|
|||
|
|
|
|||
|
|
! BulkheadConfig
|
|||
|
|
BulkheadCfg.tab.Diameter = Prumer:
|
|||
|
|
BulkheadCfg.tab.Thickness = Tlou\u0161tka:
|
|||
|
|
BulkheadCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
BulkheadCfg.tab.Generalproperties = Obecn<EFBFBD> vlastnosti
|
|||
|
|
|
|||
|
|
!CenteringRingConfig
|
|||
|
|
CenteringRingCfg.tab.Outerdiam = Vnej\u0161<36> prumer:
|
|||
|
|
CenteringRingCfg.tab.Innerdiam = Vnitrn<EFBFBD> prumer:
|
|||
|
|
CenteringRingCfg.tab.Thickness = Tlou\u0161tka:
|
|||
|
|
CenteringRingCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
CenteringRingCfg.tab.Generalproperties = Obecn<EFBFBD> vlastnosti
|
|||
|
|
|
|||
|
|
!ComponentConfigDialog
|
|||
|
|
ComponentCfgDlg.configuration = konfigurace
|
|||
|
|
ComponentCfgDlg.configuration1 =
|
|||
|
|
ComponentCfgDlg.Modify = Uprav
|
|||
|
|
|
|||
|
|
!StageConfig
|
|||
|
|
StageConfig.tab.Separation = Oddelen<EFBFBD>
|
|||
|
|
StageConfig.tab.Separation.ttip = Vlastnosti oddelen<65> stupne
|
|||
|
|
StageConfig.separation.lbl.title = Oznac kdy se m<> tento stupn oddelit:
|
|||
|
|
StageConfig.separation.lbl.plus = plus
|
|||
|
|
StageConfig.separation.lbl.seconds = sekundy
|
|||
|
|
|
|||
|
|
!EllipticalFinSetConfig
|
|||
|
|
EllipticalFinSetCfg.Nbroffins = Pocet stabiliz<69>toru:
|
|||
|
|
EllipticalFinSetCfg.Rotation = Otocen<EFBFBD>:
|
|||
|
|
EllipticalFinSetCfg.Fincant = Natocen<EFBFBD> stabiliz<69>toru:
|
|||
|
|
EllipticalFinSetCfg.Rootchord = V<EFBFBD>\u0161ka stabiliz<69>toru:
|
|||
|
|
EllipticalFinSetCfg.Height = \u0160irka stabiliz<69>toru:
|
|||
|
|
EllipticalFinSetCfg.Positionrelativeto = Pozice vzhledem k:
|
|||
|
|
EllipticalFinSetCfg.plus = plus
|
|||
|
|
EllipticalFinSetCfg.FincrossSection = Hrany stabiliz<69>toru:
|
|||
|
|
EllipticalFinSetCfg.Thickness = Tlou\u0161tka:
|
|||
|
|
EllipticalFinSetCfg.General = General
|
|||
|
|
EllipticalFinSetCfg.Generalproperties = Obecn<EFBFBD> vlastnosti
|
|||
|
|
EllipticalFinSetCfg.ttip.Fincant = <EFBFBD>hly stabiliz<69>toru jsou nakloneny vzhledem k telu rakety.
|
|||
|
|
|
|||
|
|
!FreeformFinSetConfig
|
|||
|
|
FreeformFinSetCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
FreeformFinSetCfg.tab.ttip.General = Obecn<EFBFBD> vlastnosti
|
|||
|
|
FreeformFinSetCfg.tab.Shape = Tvar
|
|||
|
|
FreeformFinSetCfg.tab.ttip.Finshape = Tvar stabiliz<69>toru
|
|||
|
|
FreeformFinSetCfg.lbl.Numberoffins = Pocet stabiliz<69>toru:
|
|||
|
|
FreeformFinSetCfg.lbl.Finrotation = Rotace stabiliz<69>toru:
|
|||
|
|
FreeformFinSetCfg.lbl.Fincant = Natocen<EFBFBD> stabiliz<69>toru:
|
|||
|
|
FreeformFinSetCfg.lbl.ttip.Fincant = <EFBFBD>hly stabiliz<69>toru jsou nakloneny vzhledem k telu rakety.
|
|||
|
|
FreeformFinSetCfg.lbl.Posrelativeto = Pozice vzhledem k:
|
|||
|
|
FreeformFinSetCfg.lbl.plus = plus
|
|||
|
|
FreeformFinSetCfg.lbl.FincrossSection = Hrany stabiliz<69>toru:
|
|||
|
|
FreeformFinSetCfg.lbl.Thickness = Tlou\u0161tka:
|
|||
|
|
! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
|
|||
|
|
FreeformFinSetConfig.lbl.doubleClick1 = Dvoj klik
|
|||
|
|
FreeformFinSetConfig.lbl.doubleClick2 = k editaci
|
|||
|
|
FreeformFinSetConfig.lbl.clickDrag = Klik a t<>hnout: Pridej a presun body
|
|||
|
|
FreeformFinSetConfig.lbl.ctrlClick = Ctrl+klik: Odstran bod
|
|||
|
|
FreeformFinSetConfig.lbl.scaleFin = Mer<EFBFBD>tko stabiliz<69>toru
|
|||
|
|
|
|||
|
|
|
|||
|
|
!InnerTubeConfig
|
|||
|
|
InnerTubeCfg.tab.Motor = Motor
|
|||
|
|
InnerTubeCfg.tab.ttip.Motor = Nastaven<EFBFBD> pripojen<65> motoru
|
|||
|
|
InnerTubeCfg.tab.Cluster = Shluk
|
|||
|
|
InnerTubeCfg.tab.ttip.Cluster = Nastaven<EFBFBD> shluku
|
|||
|
|
InnerTubeCfg.tab.Radialpos = Vzd<EFBFBD>lenost od stredu
|
|||
|
|
InnerTubeCfg.tab.ttip.Radialpos = Vzd<EFBFBD>lenost od stredu
|
|||
|
|
InnerTubeCfg.lbl.Selectclustercfg = Nastaven<EFBFBD> konfigurace shluku:
|
|||
|
|
InnerTubeCfg.lbl.TubeSep = Vzd<EFBFBD>lenost od ostatn<74>ch trubek:
|
|||
|
|
InnerTubeCfg.lbl.ttip.TubeSep = Vzd<EFBFBD>lenost od ostatn<74>ch trubek, 1.0 = dot<6F>k<EFBFBD>n<EFBFBD> se ostatn<74>ch
|
|||
|
|
InnerTubeCfg.lbl.Rotation = Rotace:
|
|||
|
|
InnerTubeCfg.lbl.ttip.Rotation = Rotace <20>hlu shlukov<6F> konfigurace
|
|||
|
|
InnerTubeCfg.lbl.Rotangle = Rotace <20>hlu shlukov<6F> konfigurace
|
|||
|
|
InnerTubeCfg.but.Splitcluster = Rozdel shluk
|
|||
|
|
InnerTubeCfg.lbl.longA1 = <html>Rozdel<65> shluka na d<>lc<6C> komponenty.<br>
|
|||
|
|
InnerTubeCfg.lbl.longA2 = Toto tak<61> duplikuje v\u0161echny komponenty pripojen<65> k t<>to vnitrn<72> trubce.
|
|||
|
|
InnerTubeCfg.but.Resetsettings = Resetuj nastaven<65>
|
|||
|
|
InnerTubeCfg.but.ttip.Resetsettings = Resetuj rozdelen<65> a rotaci na v<>choz<6F> hodnoty
|
|||
|
|
|
|||
|
|
! LaunchLugConfig
|
|||
|
|
LaunchLugCfg.lbl.Length = D<EFBFBD>lka:
|
|||
|
|
LaunchLugCfg.lbl.Outerdiam = Vnej\u0161<36> prumer:
|
|||
|
|
LaunchLugCfg.lbl.Innerdiam = Vnitrn<EFBFBD> prumer:
|
|||
|
|
LaunchLugCfg.lbl.Thickness = Tlou\u0161tka:
|
|||
|
|
LaunchLugCfg.lbl.Radialpos = Vzd<EFBFBD>lenost od stredu:
|
|||
|
|
LaunchLugCfg.lbl.Posrelativeto = Pozice vzhledem k:
|
|||
|
|
LaunchLugCfg.lbl.plus = plus
|
|||
|
|
LaunchLugCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
LaunchLugCfg.tab.Generalprop = Obecn<EFBFBD> vlastnosti
|
|||
|
|
|
|||
|
|
! MassComponentConfig
|
|||
|
|
MassComponentCfg.lbl.Mass = Hmotnost:
|
|||
|
|
MassComponentCfg.lbl.Length = D<EFBFBD>lka:
|
|||
|
|
MassComponentCfg.lbl.Diameter = Prumer:
|
|||
|
|
MassComponentCfg.lbl.PosRelativeto = Pozice vzhledem k:
|
|||
|
|
MassComponentCfg.lbl.plus = plus
|
|||
|
|
MassComponentCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
MassComponentCfg.tab.ttip.General = Obecn<EFBFBD> vlastnosti
|
|||
|
|
MassComponentCfg.tab.Radialpos = Vzd<EFBFBD>lenost od stredu
|
|||
|
|
MassComponentCfg.tab.ttip.Radialpos = Radial position configuration
|
|||
|
|
MassComponentCfg.lbl.Radialdistance = Vzd<EFBFBD>lenost od stredu:
|
|||
|
|
MassComponentCfg.lbl.Radialdirection = Smer vzdalov<6F>n<EFBFBD> se od stredu:
|
|||
|
|
MassComponentCfg.but.Reset = Reset
|
|||
|
|
|
|||
|
|
! MotorConfig
|
|||
|
|
MotorCfg.checkbox.compmotormount = Tto komponeta je pripojen<65> motoru
|
|||
|
|
MotorCfg.lbl.Motorcfg = Nastaven<EFBFBD> motoru:
|
|||
|
|
MotorCfg.but.New = Nov<EFBFBD>
|
|||
|
|
MotorCfg.lbl.Currentmotor = Soucasn<EFBFBD> motor:
|
|||
|
|
MotorCfg.lbl.Motoroverhang = Precn<EFBFBD>v<EFBFBD>n<EFBFBD> motoru:
|
|||
|
|
MotorCfg.lbl.Ignitionat = Zapalov<EFBFBD>n<EFBFBD> v:
|
|||
|
|
MotorCfg.lbl.plus = plus
|
|||
|
|
MotorCfg.lbl.seconds = sekundy
|
|||
|
|
MotorCfg.lbl.longA1 = Soucasn<EFBFBD> n<>vrh m<> pouze jeden motor.
|
|||
|
|
MotorCfg.lbl.longA2 = Stupne mohou b<>t prid<69>ny kliknut<75>m na \"Nov<6F> stupen\".
|
|||
|
|
MotorCfg.lbl.longB1 = Soucasn<EFBFBD> n<>vrh m<>
|
|||
|
|
MotorCfg.lbl.longB2 = stupnu.
|
|||
|
|
MotorCfg.but.Selectmotor = Vyber motor
|
|||
|
|
MotorCfg.but.Removemotor = Odeber motor
|
|||
|
|
MotorCfg.lbl.motorLabel = Nic
|
|||
|
|
|
|||
|
|
! NoseConeConfig
|
|||
|
|
NoseConeCfg.lbl.Noseconeshape = Tvar nosn<73>ho ku\u017Eele:
|
|||
|
|
NoseConeCfg.lbl.Shapeparam = Tvarov<EFBFBD> parametr:
|
|||
|
|
NoseConeCfg.lbl.Noseconelength = D<EFBFBD>lka nosn<73>ho ku\u017Eelu:
|
|||
|
|
NoseConeCfg.lbl.Basediam = Z<EFBFBD>kladov<EFBFBD> prumer:
|
|||
|
|
NoseConeCfg.checkbox.Automatic = Automaticky
|
|||
|
|
NoseConeCfg.lbl.Wallthickness = Tlou\u0161tka steny:
|
|||
|
|
NoseConeCfg.checkbox.Filled = Vyplneno
|
|||
|
|
NoseConeCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
NoseConeCfg.tab.ttip.General = Obecn<EFBFBD> vlastnosti
|
|||
|
|
NoseConeCfg.tab.Shoulder = Pripojen<EFBFBD>
|
|||
|
|
NoseConeCfg.tab.ttip.Shoulder = Parametry pripojen<65>
|
|||
|
|
|
|||
|
|
! ParachuteConfig
|
|||
|
|
ParachuteCfg.lbl.Canopy = Vrchl<EFBFBD>k pad<61>ku:
|
|||
|
|
ParachuteCfg.lbl.Diameter = Prumer:
|
|||
|
|
ParachuteCfg.lbl.Material = Materi<EFBFBD>l:
|
|||
|
|
ParachuteCfg.combo.MaterialModel = Materi<EFBFBD>l pad<61>ku ovlivnuje hmotnost pad<61>ku.
|
|||
|
|
ParachuteCfg.lbl.longA1 = <html>Brzdn<64> koeficient C<sub>D</sub>:
|
|||
|
|
ParachuteCfg.lbl.longB1 = <html>Brzdn<64> koeficient je vzta\u017En<45> k celkov<6F> plo\u0161e pad<61>ku.<br>
|
|||
|
|
ParachuteCfg.lbl.longB2 = Vy\u0161\u0161<36> brzdn<64> koeficient dovoluje pomalej\u0161<36> sestup.
|
|||
|
|
ParachuteCfg.lbl.longB3 = Typick<EFBFBD> hodnoty pro pad<61>k jsou 0.8.
|
|||
|
|
ParachuteCfg.but.Reset = Reset
|
|||
|
|
ParachuteCfg.lbl.Shroudlines = Pad<EFBFBD>kov<EFBFBD> \u0161nury:
|
|||
|
|
ParachuteCfg.lbl.Numberoflines = Pocet \u0161nur:
|
|||
|
|
ParachuteCfg.lbl.Linelength = D<EFBFBD>lka \u0161nur:
|
|||
|
|
ParachuteCfg.lbl.Material = Materi<EFBFBD>l:
|
|||
|
|
ParachuteCfg.lbl.Posrelativeto = Pozice vzhledem k:
|
|||
|
|
ParachuteCfg.lbl.plus = plus
|
|||
|
|
ParachuteCfg.lbl.Packedlength = D<EFBFBD>lka bal<61>ku:
|
|||
|
|
ParachuteCfg.lbl.Packeddiam = Prumer bal<61>ku:
|
|||
|
|
ParachuteCfg.lbl.Deploysat = Rozvinout v:
|
|||
|
|
ParachuteCfg.lbl.seconds = sekundy
|
|||
|
|
ParachuteCfg.lbl.Altitude = V<EFBFBD>\u0161ka:
|
|||
|
|
ParachuteCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
ParachuteCfg.tab.ttip.General = Obecn<EFBFBD> vlastnosti
|
|||
|
|
ParachuteCfg.tab.Radialpos = Vzd<EFBFBD>lenost od stredu
|
|||
|
|
ParachuteCfg.tab.ttip.Radialpos = Konfigurace stredov<6F> pozice
|
|||
|
|
ParachuteCfg.lbl.Radialdistance = Vzd<EFBFBD>lenost od stredu:
|
|||
|
|
ParachuteCfg.lbl.Radialdirection = Smer vzdalov<6F>n<EFBFBD> se od stredu:
|
|||
|
|
ParachuteCfg.but.Reset = Reset
|
|||
|
|
ParachuteCfg.lbl.plusdelay = plus
|
|||
|
|
|
|||
|
|
! ShockCordConfig
|
|||
|
|
ShockCordCfg.lbl.Shockcordlength = D<EFBFBD>lka poutac<61> \u0161nury:
|
|||
|
|
ShockCordCfg.lbl.Shockcordmaterial = Materi<EFBFBD>l poutac<61> \u0161nury:
|
|||
|
|
ShockCordCfg.lbl.Posrelativeto = Pozice vzhledem k:
|
|||
|
|
ShockCordCfg.lbl.plus = plus
|
|||
|
|
ShockCordCfg.lbl.Packedlength = D<EFBFBD>lka bal<61>ku:
|
|||
|
|
ShockCordCfg.lbl.Packeddiam = Prumer bal<61>ku:
|
|||
|
|
ShockCordCfg.tab.General = General
|
|||
|
|
ShockCordCfg.tab.ttip.General = Obecn<EFBFBD> vlastnosti
|
|||
|
|
|
|||
|
|
!SleeveConfig
|
|||
|
|
SleeveCfg.tab.Outerdiam = Vnej\u0161<36> prumer:
|
|||
|
|
SleeveCfg.tab.Innerdiam = Vnitrn<EFBFBD> prumer:
|
|||
|
|
SleeveCfg.tab.Wallthickness = Tlou\u0161tka zdi:
|
|||
|
|
SleeveCfg.tab.Length = D<EFBFBD>lka:
|
|||
|
|
SleeveCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
SleeveCfg.tab.Generalproperties = Obecn<EFBFBD> vlastnosti
|
|||
|
|
|
|||
|
|
! StreamerConfig
|
|||
|
|
StreamerCfg.lbl.Striplength = D<EFBFBD>lka pruhu:
|
|||
|
|
StreamerCfg.lbl.Stripwidth = \u0160<36>rka pruhu:
|
|||
|
|
StreamerCfg.lbl.Striparea = Plocha pruhu:
|
|||
|
|
StreamerCfg.lbl.Aspectratio = Pomer pruhu:
|
|||
|
|
StreamerCfg.lbl.Material = Materi<EFBFBD>l:
|
|||
|
|
StreamerCfg.combo.ttip.MaterialModel = Materi<EFBFBD>l komponenty m<> vliv na v<>hu komponenty.
|
|||
|
|
StreamerCfg.lbl.longA1 = <html>Brzdn<64> koeficient C<sub>D</sub>:
|
|||
|
|
StreamerCfg.lbl.longB1 = <html>Brzdn<64> koeficient se vztahuje k celkov<6F> plose stuhy.<br>
|
|||
|
|
StreamerCfg.lbl.longB2 = Vy\u0161\u0161<36> brzdn<64> koeficient dovoluje pomalej\u0161<36> sestup.
|
|||
|
|
StreamerCfg.lbl.Automatic = Automatick<EFBFBD>
|
|||
|
|
StreamerCfg.lbl.longC1 = Brzdn<EFBFBD> koeficient se vztahuje k celkov<6F> plose stuhy.
|
|||
|
|
StreamerCfg.lbl.Posrelativeto = Pozice vzhledem k:
|
|||
|
|
StreamerCfg.lbl.plus = plus
|
|||
|
|
StreamerCfg.lbl.Packedlength = D<EFBFBD>lka bal<61>ku:
|
|||
|
|
StreamerCfg.lbl.Packeddiam = Prumer bal<61>ku:
|
|||
|
|
StreamerCfg.lbl.Deploysat = Rozvinout v:
|
|||
|
|
StreamerCfg.lbl.seconds = sekundy
|
|||
|
|
StreamerCfg.lbl.Altitude = Nadmorsk<EFBFBD> v<>\u0161ka:
|
|||
|
|
StreamerCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
StreamerCfg.tab.ttip.General = Obecn<EFBFBD> vlastnosti
|
|||
|
|
StreamerCfg.tab.Radialpos = Vzd<EFBFBD>lenost od stredu
|
|||
|
|
StreamerCfg.tab.ttip.Radialpos = Nastaven<EFBFBD> pozice od stredu
|
|||
|
|
StreamerCfg.lbl.Radialdistance = Vzd<EFBFBD>lenost od stredu:
|
|||
|
|
StreamerCfg.lbl.Radialdirection = Smer vzdalov<6F>n<EFBFBD> se od stredu:
|
|||
|
|
StreamerCfg.but.Reset = Reset
|
|||
|
|
StreamerCfg.lbl.plusdelay = plus
|
|||
|
|
|
|||
|
|
! ThicknessRingComponentConfig
|
|||
|
|
ThicknessRingCompCfg.tab.Outerdiam = Vnej\u0161<36> prumer:
|
|||
|
|
ThicknessRingCompCfg.tab.Innerdiam = Vnitrn<EFBFBD> prumer:
|
|||
|
|
ThicknessRingCompCfg.tab.Wallthickness = Tlou\u0161tka zdi:
|
|||
|
|
ThicknessRingCompCfg.tab.Length = D<EFBFBD>lka:
|
|||
|
|
ThicknessRingCompCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
ThicknessRingCompCfg.tab.Generalprop = Obecn<EFBFBD> vlastnosti
|
|||
|
|
|
|||
|
|
! TransitionConfig
|
|||
|
|
TransitionCfg.lbl.Transitionshape = Tvar prechodu trupu:
|
|||
|
|
TransitionCfg.checkbox.Clipped = Zkr<EFBFBD>cen<EFBFBD>
|
|||
|
|
TransitionCfg.lbl.Shapeparam = Parametr tvaru:
|
|||
|
|
TransitionCfg.lbl.Transitionlength = D<EFBFBD>lka prechodu trupu:
|
|||
|
|
TransitionCfg.lbl.Forediam = Pr<EFBFBD>dov<EFBFBD> prumer prechodu trupu:
|
|||
|
|
TransitionCfg.checkbox.Automatic = Automatick<EFBFBD>
|
|||
|
|
TransitionCfg.lbl.Aftdiam = Z<EFBFBD>dov<EFBFBD> prumer:
|
|||
|
|
TransitionCfg.lbl.Wallthickness = Tlou\u0161tka steny:
|
|||
|
|
TransitionCfg.checkbox.Filled = Vyplneno
|
|||
|
|
TransitionCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
TransitionCfg.tab.Generalproperties = Obecn<EFBFBD> vlastnosti
|
|||
|
|
TransitionCfg.tab.Shoulder = Pripojen<EFBFBD>
|
|||
|
|
TransitionCfg.tab.Shoulderproperties = Parametry pripojen<65>
|
|||
|
|
|
|||
|
|
! TrapezoidFinSetConfig
|
|||
|
|
TrapezoidFinSetCfg.lbl.Nbroffins = Pocet stabiliz<69>toru:
|
|||
|
|
TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Pocet kr<6B>d<EFBFBD>lek tvor<6F>c<EFBFBD> stabiliz<69>tor.
|
|||
|
|
TrapezoidFinSetCfg.lbl.Finrotation = Rotace stabiliz<69>toru:
|
|||
|
|
TrapezoidFinSetCfg.lbl.ttip.Finrotation = <EFBFBD>hel prvn<76>ho krid<69>lka v stabiliz<69>toru.
|
|||
|
|
TrapezoidFinSetCfg.lbl.Fincant = Natocen<EFBFBD> stabiliz<69>toru:
|
|||
|
|
TrapezoidFinSetCfg.lbl.ttip.Fincant = <EFBFBD>hly stabiliz<69>toru jsou nakloneny vzhledem k telu rakety.
|
|||
|
|
TrapezoidFinSetCfg.lbl.Rootchord = Koren kr<6B>dla:
|
|||
|
|
TrapezoidFinSetCfg.lbl.Tipchord = Konec kr<6B>dla:
|
|||
|
|
TrapezoidFinSetCfg.lbl.Height = V<EFBFBD>\u0161ka:
|
|||
|
|
TrapezoidFinSetCfg.lbl.Sweeplength = D<EFBFBD>lka skosen<65>:
|
|||
|
|
TrapezoidFinSetCfg.lbl.Sweepangle = <EFBFBD>hel skosen<65>:
|
|||
|
|
TrapezoidFinSetCfg.lbl.FincrossSection = Hrany stabiliz<69>toru:
|
|||
|
|
TrapezoidFinSetCfg.lbl.Thickness = Tlou\u0161tka:
|
|||
|
|
TrapezoidFinSetCfg.lbl.Posrelativeto = Pozice vzhledem k:
|
|||
|
|
TrapezoidFinSetCfg.lbl.plus = plus
|
|||
|
|
TrapezoidFinSetCfg.tab.General = Obecn<EFBFBD>
|
|||
|
|
TrapezoidFinSetCfg.tab.Generalproperties = Obecn<EFBFBD> vlastnosti
|
|||
|
|
|
|||
|
|
!MotorConfigurationModel
|
|||
|
|
MotorCfgModel.Editcfg = Editace konfigurace
|
|||
|
|
|
|||
|
|
! StorageOptionChooser
|
|||
|
|
StorageOptChooser.lbl.Simdatatostore = Simulacn<EFBFBD> data k ulo\u017Een<65>:
|
|||
|
|
StorageOptChooser.rdbut.Allsimdata = V\u0161echny data ze simulace
|
|||
|
|
StorageOptChooser.lbl.longA1 = <html>Ulo\u017E<37> v\u0161echny simulacn<63> data.<br>
|
|||
|
|
StorageOptChooser.lbl.longA2 = V<EFBFBD>sledek mu\u017Ee vy<76>stit ve velmi velk<6C> soubory!
|
|||
|
|
StorageOptChooser.rdbut.Every = Ka\u017Ed<45>
|
|||
|
|
StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>
|
|||
|
|
StorageOptChooser.lbl.longB2 = Vet\u0161<36> hodnoty vy<76>st<73> v men\u0161<36> soubory.
|
|||
|
|
StorageOptChooser.lbl.seconds = sekundy
|
|||
|
|
StorageOptChooser.rdbut.Onlyprimfig = Pouze hlavn<76> grafy
|
|||
|
|
StorageOptChooser.lbl.longC1 = <html>Ulo\u017E pouze hodnoty uk<75>zan<61> v prehledu.<br>
|
|||
|
|
StorageOptChooser.lbl.longC2 = This results in the smallest files.
|
|||
|
|
StorageOptChooser.checkbox.Compfile = Zkomprimovat soubor
|
|||
|
|
StorageOptChooser.lbl.UsingComp = Pou\u017Eit<69>m komprese se v<>znamne redukuje velikost souboru.
|
|||
|
|
StorageOptChooser.lbl.longD1 = Odhad jak velk<6C> bude v<>sledn<64> soubor se stavaj<61>c<EFBFBD>m nastaven<65>m.
|
|||
|
|
StorageOptChooser.ttip.Saveopt = Ulo\u017Eit nastaven<65>
|
|||
|
|
StorageOptChooser.lbl.Estfilesize = Odhadovan<EFBFBD> velikost souboru:
|
|||
|
|
StorageOptChooser.lbl.Saveopt = Ulo\u017Eit nastaven<65>
|
|||
|
|
|
|||
|
|
! ThrustCurveMotorSelectionPanel
|
|||
|
|
TCMotorSelPan.lbl.Selrocketmotor = Vyber raketov<6F> motor:
|
|||
|
|
TCMotorSelPan.checkbox.hideSimilar = Schovej velmi podobn<62> v<>konov<6F> krivky
|
|||
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Uka\u017E v\u0161echny motory
|
|||
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Uka\u017E motory s prumerem men\u0161<36>m ne\u017E toto uchycen<65> motoru
|
|||
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Uka\u017E motory se stejn<6A>m prumerem jako toto uchycen<65> motoru
|
|||
|
|
TCMotorSelPan.lbl.Motormountdia = Prumer uchycen<65> motoru:
|
|||
|
|
TCMotorSelPan.lbl.Search = Hledej:
|
|||
|
|
TCMotorSelPan.lbl.Selectthrustcurve = Vyber v<>konovou krivku:
|
|||
|
|
TCMotorSelPan.lbl.Ejectionchargedelay = Oddelovac<EFBFBD> zpo\u017Eden<65>:
|
|||
|
|
TCMotorSelPan.equalsIgnoreCase.None = Nic
|
|||
|
|
TCMotorSelPan.lbl.NumberofsecondsorNone = (Pocet sekund nebo \"Nic\")
|
|||
|
|
TCMotorSelPan.lbl.Totalimpulse = Celkov<EFBFBD> impulse:
|
|||
|
|
TCMotorSelPan.lbl.Avgthrust = Prumern<EFBFBD> tah:
|
|||
|
|
TCMotorSelPan.lbl.Maxthrust = Maxim<EFBFBD>ln<EFBFBD> tah:
|
|||
|
|
TCMotorSelPan.lbl.Burntime = Doba horen<65>:
|
|||
|
|
TCMotorSelPan.lbl.Launchmass = Hmotnost pri startu:
|
|||
|
|
TCMotorSelPan.lbl.Emptymass = Pr<EFBFBD>zdn<EFBFBD> hmotnost:
|
|||
|
|
TCMotorSelPan.lbl.Datapoints = Datov<EFBFBD> body:
|
|||
|
|
TCMotorSelPan.lbl.Digest = V<EFBFBD>ber:
|
|||
|
|
TCMotorSelPan.title.Thrustcurve = V<EFBFBD>konov<EFBFBD> krivka:
|
|||
|
|
TCMotorSelPan.title.Thrust = Tah
|
|||
|
|
TCMotorSelPan.delayBox.None = Nic
|
|||
|
|
|
|||
|
|
|
|||
|
|
! PlotDialog
|
|||
|
|
PlotDialog.title.Flightdataplot = Flight data plot
|
|||
|
|
PlotDialog.Chart.Simulatedflight = Simulovan<EFBFBD> let
|
|||
|
|
PlotDialog.CheckBox.Showdatapoints = Uka\u017E datov<6F> body
|
|||
|
|
PlotDialog.lbl.Chart = Kliknout a t<>hnout dolu a doprava zvet\u0161en<65> nahoru a vlevo zmen\u0161en<65>
|
|||
|
|
|
|||
|
|
|
|||
|
|
! "main" prefix is used for the main application dialog
|
|||
|
|
|
|||
|
|
# FIXME: Rename the description keys
|
|||
|
|
|
|||
|
|
main.menu.file = Soubor
|
|||
|
|
main.menu.file.desc = Operace se souborem
|
|||
|
|
main.menu.file.new = Nov<EFBFBD>
|
|||
|
|
main.menu.file.new.desc = Vytvorit nov<6F> n<>vrh rakety
|
|||
|
|
main.menu.file.open = Otevr<EFBFBD>t...
|
|||
|
|
BasicFrame.item.Openrocketdesign = Otevr<EFBFBD>t n<>vrh rakety
|
|||
|
|
main.menu.file.openExample = Otevr<EFBFBD>t uk<75>zku...
|
|||
|
|
BasicFrame.item.Openexamplerocketdesign = Otevr<EFBFBD>t uk<75>zkov<6F> n<>vrh rakety
|
|||
|
|
main.menu.file.save = Ulo\u017Eit
|
|||
|
|
BasicFrame.item.SavecurRocketdesign = Ulo\u017Eit soucasn<73> n<>vrh rakety
|
|||
|
|
main.menu.file.saveAs = Ulo\u017Eit jako...
|
|||
|
|
BasicFrame.item.SavecurRocketdesnewfile = Ulo\u017Eit soucasn<73> n<>vrh rakety do nov<6F>ho souboru
|
|||
|
|
main.menu.file.print = Vytisknout / exportovat do PDF...
|
|||
|
|
main.menu.file.print.desc = Vytisknout nebo exportovat do PDF jako Print or save as PDF the parts list and fin templates
|
|||
|
|
main.menu.file.close = Zavr<EFBFBD>t
|
|||
|
|
BasicFrame.item.Closedesign = Ulo\u017Eit soucasn<73> n<>vrh rakety
|
|||
|
|
main.menu.file.quit = Konec
|
|||
|
|
BasicFrame.item.Quitprogram = Ukonci progrem
|
|||
|
|
|
|||
|
|
main.menu.edit = Edituj
|
|||
|
|
BasicFrame.menu.Rocketedt = Editace rakety
|
|||
|
|
main.menu.edit.undo = Zpet
|
|||
|
|
main.menu.edit.undo.desc = Vr<EFBFBD>tit zpet predchoz<6F> akci
|
|||
|
|
main.menu.edit.redo = Znovu
|
|||
|
|
main.menu.edit.redo.desc = Znovu predchoz<6F> operaci
|
|||
|
|
main.menu.edit.cut = Vyjmout
|
|||
|
|
main.menu.edit.copy = Kop<EFBFBD>rovat
|
|||
|
|
main.menu.edit.paste = Vlo\u017Eit
|
|||
|
|
main.menu.edit.delete = Smazat
|
|||
|
|
main.menu.edit.resize = Mer<EFBFBD>tko...
|
|||
|
|
main.menu.edit.resize.desc = Mer<EFBFBD>tko c<>st<73> n<>vrhu rakety
|
|||
|
|
main.menu.edit.preferences = Nastaven<EFBFBD>
|
|||
|
|
main.menu.edit.preferences.desc = Nastaven<EFBFBD> aplikace
|
|||
|
|
|
|||
|
|
main.menu.analyze = Anal\u017E<37>za
|
|||
|
|
main.menu.analyze.desc = Anal<EFBFBD>za rakety
|
|||
|
|
main.menu.analyze.componentAnalysis = Anal<EFBFBD>za komponent
|
|||
|
|
main.menu.analyze.componentAnalysis.desc = Analyzuj c<>sti rakety samostatne
|
|||
|
|
main.menu.analyze.optimization = Optimalizace rakety
|
|||
|
|
main.menu.analyze.optimization.desc = Obecn<EFBFBD> n<>vrh optimalizace rakety
|
|||
|
|
|
|||
|
|
main.menu.help = Pomoc
|
|||
|
|
main.menu.help.desc = Informace o programu OpenRocket
|
|||
|
|
main.menu.help.tours = Prohl<EFBFBD>dky z pruvodcem
|
|||
|
|
main.menu.help.tours.desc = Uka\u017E prohl<68>dku programu OpenRocket
|
|||
|
|
main.menu.help.license = Licence
|
|||
|
|
main.menu.help.license.desc = Informaci o licenci OpenRocket
|
|||
|
|
main.menu.help.bugReport = Hl<EFBFBD>\u0161en<65> chyb
|
|||
|
|
main.menu.help.bugReport.desc = Informace o hl<68>\u0161en<65> chyb v OpenRocket
|
|||
|
|
main.menu.help.debugLog = Informace o laden<65>
|
|||
|
|
main.menu.help.debugLog.desc = Uka\u017E informace o laden<65> OpenRocket
|
|||
|
|
main.menu.help.about = O programu
|
|||
|
|
main.menu.help.about.desc = Detaily autorsk<73>ch pr<70>v k OpenRocket
|
|||
|
|
|
|||
|
|
main.menu.debug = laden<EFBFBD>
|
|||
|
|
main.menu.debug.whatisthismenu = Co je v tomto menu?
|
|||
|
|
main.menu.debug.createtestrocket = Udelej test rakety
|
|||
|
|
|
|||
|
|
! database
|
|||
|
|
! Translate here all material database
|
|||
|
|
!
|
|||
|
|
|
|||
|
|
! Material database
|
|||
|
|
! BULK_MATERIAL
|
|||
|
|
Databases.materials.Acrylic = Akryl
|
|||
|
|
Databases.materials.Aluminum = Hlin<EFBFBD>k
|
|||
|
|
Databases.materials.Balsa = Balza
|
|||
|
|
Databases.materials.Basswood = L<EFBFBD>pa
|
|||
|
|
Databases.materials.Birch = Br<EFBFBD>za
|
|||
|
|
Databases.materials.Brass = Mosaz
|
|||
|
|
Databases.materials.Cardboard = Kart<EFBFBD>n
|
|||
|
|
Databases.materials.Carbonfiber = Vystu\u017Een<65> kart<72>n
|
|||
|
|
Databases.materials.Cork = Korek
|
|||
|
|
Databases.materials.DepronXPS = Depron (XPS)
|
|||
|
|
Databases.materials.Fiberglass = Skeln<EFBFBD> vl<76>kno
|
|||
|
|
Databases.materials.Kraftphenolic = Kraft phenolic
|
|||
|
|
Databases.materials.Maple = Javor
|
|||
|
|
Databases.materials.Paperoffice = Pap<EFBFBD>r (kancel<65>rsk<73>)
|
|||
|
|
Databases.materials.Pine = Borovice
|
|||
|
|
Databases.materials.Plywoodbirch = Prekli\u017Eka (briza)
|
|||
|
|
Databases.materials.PolycarbonateLexan = Polykarbon<EFBFBD>t (Lexan)
|
|||
|
|
Databases.materials.Polystyrene = Polystyr<EFBFBD>n
|
|||
|
|
Databases.materials.PVC = PVC
|
|||
|
|
Databases.materials.Spruce = Smrk
|
|||
|
|
Databases.materials.Steel = Ocel
|
|||
|
|
Databases.materials.StyrofoamgenericEPS = Styrofoam (obecn<63> EPS)
|
|||
|
|
Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"modr<64> pena\" (XPS)
|
|||
|
|
Databases.materials.Titanium = Titan
|
|||
|
|
Databases.materials.Quantumtubing = Quantum tubing
|
|||
|
|
Databases.materials.BlueTube = Blue tube
|
|||
|
|
!SURFACE_MATERIAL
|
|||
|
|
Databases.materials.Ripstopnylon = Ripstoponov<EFBFBD> nylon
|
|||
|
|
Databases.materials.Mylar = Mylar
|
|||
|
|
Databases.materials.Polyethylenethin = Polyethyl<EFBFBD>n (tenk<6E>)
|
|||
|
|
Databases.materials.Polyethyleneheavy = Polyethyl<EFBFBD>n (te\u017Ek<45>)
|
|||
|
|
Databases.materials.Silk = Hedv<EFBFBD>b<EFBFBD>
|
|||
|
|
Databases.materials.Paperoffice = Pap<EFBFBD>r (kancel<65>rsk<73>)
|
|||
|
|
Databases.materials.Cellophane = Celof<EFBFBD>n
|
|||
|
|
Databases.materials.Crepepaper = Celul<EFBFBD>rn<EFBFBD> pap<61>r
|
|||
|
|
! LINE_MATERIAL
|
|||
|
|
Databases.materials.Threadheavy-duty = Vl<EFBFBD>kno (vysoce odoln<6C>)
|
|||
|
|
Databases.materials.Elasticcordround2mm = Elastick<EFBFBD> \u0161nura (round 2mm, 1/16 in)
|
|||
|
|
Databases.materials.Elasticcordflat6mm = Elastick<EFBFBD> \u0161nura (flat 6mm, 1/4 in)
|
|||
|
|
Databases.materials.Elasticcordflat12mm = Elastick<EFBFBD> \u0161nura (flat 12mm, 1/2 in)
|
|||
|
|
Databases.materials.Elasticcordflat19mm = Elastick<EFBFBD> \u0161nura (flat 19mm, 3/4 in)
|
|||
|
|
Databases.materials.Elasticcordflat25mm = Elastick<EFBFBD> \u0161nura (flat 25mm, 1 in)
|
|||
|
|
Databases.materials.Braidednylon2mm = Spleten<EFBFBD> nylon (2 mm, 1/16 in)
|
|||
|
|
Databases.materials.Braidednylon3mm = Spleten<EFBFBD> nylon (3 mm, 1/8 in)
|
|||
|
|
Databases.materials.Tubularnylon11mm = Trubkovit<EFBFBD> nylon (11 mm, 7/16 in)
|
|||
|
|
Databases.materials.Tubularnylon14mm = Trubkovit<EFBFBD> nylon (14 mm, 9/16 in)
|
|||
|
|
Databases.materials.Tubularnylon25mm = Trubkovit<EFBFBD> nylon (25 mm, 1 in)
|
|||
|
|
|
|||
|
|
! ExternalComponent
|
|||
|
|
ExternalComponent.Rough = drsn<EFBFBD>
|
|||
|
|
ExternalComponent.Unfinished = nedokoncen<EFBFBD>
|
|||
|
|
ExternalComponent.Regularpaint = norm<EFBFBD>lne natren<65>
|
|||
|
|
ExternalComponent.Smoothpaint = jemne natren<65>
|
|||
|
|
ExternalComponent.Polished = vyle\u0161ten<65>
|
|||
|
|
|
|||
|
|
! LineStyle
|
|||
|
|
LineStyle.Solid = pevn<EFBFBD>
|
|||
|
|
LineStyle.Dashed = c<EFBFBD>rkovan<EFBFBD>
|
|||
|
|
LineStyle.Dotted = teckovan<EFBFBD>
|
|||
|
|
LineStyle.Dash-dotted = tecko-c<>rkovan<61>
|
|||
|
|
LineStyle.Defaultstyle = V<EFBFBD>choz<EFBFBD> styl
|
|||
|
|
|
|||
|
|
! Shape
|
|||
|
|
Shape.Conical = Ku\u017Eelovit<69>
|
|||
|
|
Shape.Conical.desc1 = Ku\u017Eelovit<69> pr<70>dov<6F> kryt m<> profil jako troj<6F>heln<6C>k.
|
|||
|
|
Shape.Conical.desc2 = Ku\u017Eel m<> rovn<76> strany.
|
|||
|
|
Shape.Ogive = Obloukovit<EFBFBD>
|
|||
|
|
Shape.Ogive.desc1 = Profil pr<70>dov<6F>ho krytu ve tvaru lomen<65>ho oblouku tvor<6F> <20>sek kru\u017Enice. Tvarov<6F> parametr o hodnote 1 urcuje <b>tecnu lomen<65>ho oblouku</b>, kter<65> plynule od oblouku prech<63>z<EFBFBD> jako telo rakety , hodota men\u0161<36> ne\u017E 1 urcuje <b>secnu lomen<65>ho oblouku</b>.
|
|||
|
|
Shape.Ogive.desc2 = Profil pr<70>dov<6F>ho krytu ve tvaru lomen<65>ho oblouku tvor<6F> <20>sek kru\u017Enice. Tvarov<6F> parametr o hodnote 1 urcuje <b>tecnu lomen<65>ho oblouku</b>, kter<65> plynule od oblouku prech<63>z<EFBFBD> jako telo rakety na z<>d, hodota men\u0161<36> ne\u017E 1 urcuje <b>secnu lomen<65>ho oblouku</b>.
|
|||
|
|
Shape.Ellipsoid = Eliptyck<EFBFBD>
|
|||
|
|
Shape.Ellipsoid.desc1 = Eliptick<EFBFBD> pr<70>dov<6F> kryt m<> profil jako polovina epilpsy a hlavn<76>mi osamy jsou 2×<i>d<>lka</i> a <i>prumer</i>.
|
|||
|
|
Shape.Ellipsoid.desc2 = Eliptick<EFBFBD> pr<70>dov<6F> kryt m<> profil jako polovina epilpsy a hlavn<76>mi osamy jsou 2×<i>d<>lka</i> a <i>prumer</i>. Pokud prechod nen<65> or<6F>znut, pak je profi roz\u0161<36>ren v centru odpov<6F>daj<61>c<EFBFBD>m polomeru.
|
|||
|
|
Shape.Powerseries = Mocnin<EFBFBD> rada
|
|||
|
|
Shape.Powerseries.desc1 = Pr<EFBFBD>dov<EFBFBD> kryt ve tvaru mocnin<69> rady m<> profil <i>r<>diusu</i> × (<i>x</i> / <i>d<>lka</i>)<sup><i>k</i></sup> kde <i>k</i> je tvarov<6F> parametr. Pro <i>k</i>=0.5 je to <b>\u00BD-power</b> nebo <b>parabolick<63></b> pr<70>dov<6F> kryt, pro <i>k</i>=0.75 a <b>\u00BE-power</b>, a pro <i>k</i>=1 a <b>ku\u017Eelovit<69></b> pr<70>dov<6F> kryt.
|
|||
|
|
Shape.Powerseries.desc2 = Prechod trupu ve tvaru mocnin<69> rady m<> profil <i>r<>diusu</i> × (<i>x</i> / <i>d<>lka</i>)<sup><i>k</i></sup> kde <i>k</i> je tvarov<6F> parametr. Pro <i>k</i>=0.5 je prechod trupu <b>\u00BD-power</b> nebo <b>parabola</b>, pro <i>k</i>=0.75 a <b>\u00BE-power</b>, a pro <i>k</i>=1 <b>ku\u017Eel</b>.
|
|||
|
|
Shape.Parabolicseries = Parabola
|
|||
|
|
Shape.Parabolicseries.desc1 = Parabolick<EFBFBD> pr<70>dov<6F> kryt m<> profil paraboly. Tvarov<6F> parametr definuje <20>sek paraboly, kter<65> je vyu\u017Eit. Tvarov<6F> parametr 1.0 produkuje <b>plnou parabolu</b> kde telov<6F> trubka je jej<65> tecnou, 0.75 produkuje <b>3/4 parabolu</b>, 0.5 produkuje <b>1/2 parabolu</b> a 0 produkuje <b>ku\u017Eelovit<69></b> pr<70>dov<6F> kryt.
|
|||
|
|
Shape.Parabolicseries.desc2 = Parabolick<EFBFBD> prechod trupu m<> profil paraboly. Tvarov<6F> parametr definuje <20>sek paraboly, kter<65> je vyu\u017Eit. Tvarov<6F> parametr 1.0 produkuje <b>plnou parabolu</b> kde telov<6F> trubka je jej<65> tecnou na zadn<64> c<>sti, 0.75 produkuje <b>3/4 parabolu</b>, 0.5 produkuje <b>1/2 parabolu</b> a 0 produkuje <b>ku\u017Eelovit<69></b> prechod trupu.
|
|||
|
|
Shape.Haackseries = Haack
|
|||
|
|
Shape.Haackseries.desc1 = Haackov<EFBFBD> pr<70>dov<6F> kryt je navr\u017Een pro minimalizov<6F>n<EFBFBD> aerodynamick<63>ho odporu. Tvarov<6F> parametr 0 produkuje <b>LD-Haack</b> nebo <b>Von Karmanuv</b> pr<70>dov<6F> kryz, kter<65> minimalizuje aerodynamick<63> odpor pro pevne danou d<>lku a prumer, zat<61>mco hodnota 0.333 produkuje <b>LV-Haack</b> pr<70>dov<6F> kryt, kter<65> minimalizuje aerodynamick<63> odpor pro pevn\u0161 danou d<>lku a objem.
|
|||
|
|
Shape.Haackseries.desc2 = Haackov<EFBFBD> <i>pr<70>dov<6F> kryt</i> je navr\u017Een pro minimalizov<6F>n<EFBFBD> aerodynamick<63>ho odporu. Tyto prechody trupu jsou jeho ekvivalenty, ale nemus<75> mit nutne optim<69>ln<6C> aerodynamick<63> odpor vzduchu pro prechod trupu. Tvarov<6F> parametr 0 produkuje <b>LD-Haack</b> nebo <b>Von Karmanuv</b> tvar, zat<61>mco hodnota 0.333 produkuje tvar<b>LV-Haack</b>.
|
|||
|
|
|
|||
|
|
|
|||
|
|
! RocketComponent
|
|||
|
|
RocketComponent.Position.TOP = Vrchol rodicovsk<73> komponenty
|
|||
|
|
RocketComponent.Position.MIDDLE = Stred rodicovsk<73> komponenty
|
|||
|
|
RocketComponent.Position.BOTTOM = Spodek rodicovsk<73> komponenty
|
|||
|
|
RocketComponent.Position.AFTER = Za rodicovskou komponentou
|
|||
|
|
RocketComponent.Position.ABSOLUTE = \u0160picka nosn<73>ho ku\u017Eelu
|
|||
|
|
|
|||
|
|
! LaunchLug
|
|||
|
|
LaunchLug.Launchlug = Vypou\u0161tec<65> oko
|
|||
|
|
! NoseCone
|
|||
|
|
NoseCone.NoseCone = Nosn<EFBFBD> ku\u017Eel
|
|||
|
|
! Transition
|
|||
|
|
Transition.Transition = Prechod
|
|||
|
|
!Stage
|
|||
|
|
Stage.Stage = Stupen
|
|||
|
|
|
|||
|
|
Stage.SeparationEvent.UPPER_IGNITION = Horn<EFBFBD> stupen zap<61>len<65> motoru
|
|||
|
|
Stage.SeparationEvent.IGNITION = Soucasn<EFBFBD> stupen zap<61>len<65> motoru
|
|||
|
|
Stage.SeparationEvent.BURNOUT = Current stage motor burnout
|
|||
|
|
Stage.SeparationEvent.EJECTION = Current stage ejection charge
|
|||
|
|
Stage.SeparationEvent.LAUNCH = Vypust
|
|||
|
|
Stage.SeparationEvent.NEVER = Nikdy
|
|||
|
|
|
|||
|
|
! BodyTube
|
|||
|
|
BodyTube.BodyTube = Telo rakety
|
|||
|
|
! TubeCoupler
|
|||
|
|
TubeCoupler.TubeCoupler = Spojen<EFBFBD> trubic
|
|||
|
|
!InnerTube
|
|||
|
|
InnerTube.InnerTube = Vnitrn<EFBFBD> trubice
|
|||
|
|
! TrapezoidFinSet
|
|||
|
|
TrapezoidFinSet.TrapezoidFinSet = Lichobe\u017En<45>kov<6F> stabiliz<69>tory
|
|||
|
|
! FreeformFinSet
|
|||
|
|
FreeformFinSet.FreeformFinSet = Volno tvarov<6F> stabiliz<69>tory
|
|||
|
|
!MassComponent
|
|||
|
|
MassComponent.MassComponent = Hmotnost komponenty
|
|||
|
|
! Parachute
|
|||
|
|
Parachute.Parachute = Pad<EFBFBD>k
|
|||
|
|
! ShockCord
|
|||
|
|
ShockCord.ShockCord = Poutac<EFBFBD> \u0160nura
|
|||
|
|
! Bulkhead
|
|||
|
|
Bulkhead.Bulkhead = Prep<EFBFBD>\u017Eka
|
|||
|
|
|
|||
|
|
!Rocket
|
|||
|
|
Rocket.motorCount.Nomotor = [\u017D<37>dn<64> motory]
|
|||
|
|
Rocket.compname.Rocket = Raketa
|
|||
|
|
|
|||
|
|
!MotorMount
|
|||
|
|
MotorMount.IgnitionEvent.AUTOMATIC = Automatick<EFBFBD> (vypu\u0161ten<65> nebo vyhozen<65> predchoz<6F>ho stupne)
|
|||
|
|
MotorMount.IgnitionEvent.LAUNCH = Vypu\u0161ten<65>
|
|||
|
|
MotorMount.IgnitionEvent.EJECTION_CHARGE = Prvn<EFBFBD> vypu\u0161ten<65> nebo vyhozen<65> predchoz<6F>ho stupne
|
|||
|
|
MotorMount.IgnitionEvent.BURNOUT = Prvn<EFBFBD> vyhoren<65> predchoz<6F>ho stupne
|
|||
|
|
MotorMount.IgnitionEvent.NEVER = Nikdy
|
|||
|
|
|
|||
|
|
!ComponentIcons
|
|||
|
|
ComponentIcons.Nosecone = Celn<EFBFBD> ku\u017Eel
|
|||
|
|
ComponentIcons.Bodytube = Telov<EFBFBD> trubka
|
|||
|
|
ComponentIcons.Transition = Prechod trupu
|
|||
|
|
ComponentIcons.Trapezoidalfinset = Lichobe\u017En<45>kov<6F> stabiliz<69>tory
|
|||
|
|
ComponentIcons.Ellipticalfinset = Eliptick<EFBFBD> stabiliz<69>tory
|
|||
|
|
ComponentIcons.Freeformfinset = Volno tvarov<6F> stabiliz<69>tory
|
|||
|
|
ComponentIcons.Launchlug = Vypou\u0161tec<65> oko
|
|||
|
|
ComponentIcons.Innertube = Vnitrn<EFBFBD> trubka
|
|||
|
|
ComponentIcons.Tubecoupler = Spojen<EFBFBD> trubic
|
|||
|
|
ComponentIcons.Centeringring = Trupov<EFBFBD> prep<65>\u017Eka
|
|||
|
|
ComponentIcons.Bulkhead = Prep<EFBFBD>\u017Eka
|
|||
|
|
ComponentIcons.Engineblock = Blok motoru
|
|||
|
|
ComponentIcons.Parachute = Pad<EFBFBD>k
|
|||
|
|
ComponentIcons.Streamer = Brzd<EFBFBD>c<EFBFBD> prou\u017Eek
|
|||
|
|
ComponentIcons.Shockcord = Poutac<EFBFBD> \u0161nura
|
|||
|
|
ComponentIcons.Masscomponent = Hmotnost komponenty
|
|||
|
|
ComponentIcons.disabled = (zak<61>zan<61>)
|
|||
|
|
|
|||
|
|
! StageAction
|
|||
|
|
StageAction.Stage = Stupen
|
|||
|
|
|
|||
|
|
! RecoveryDevice
|
|||
|
|
RecoveryDevice.DeployEvent.LAUNCH = Vypu\u0161ten<65> (plus NN sekund)
|
|||
|
|
RecoveryDevice.DeployEvent.EJECTION = Prvn<EFBFBD> vyhoren<65> tohoto stupne
|
|||
|
|
RecoveryDevice.DeployEvent.APOGEE = Vrchol
|
|||
|
|
RecoveryDevice.DeployEvent.ALTITUDE = Konkr<EFBFBD>tn<EFBFBD> v<>\u0161ka behem sestupu
|
|||
|
|
RecoveryDevice.DeployEvent.NEVER = Nikdy
|
|||
|
|
|
|||
|
|
! FlightEvent
|
|||
|
|
FlightEvent.Type.LAUNCH = Vypu\u0161ten<65>
|
|||
|
|
FlightEvent.Type.IGNITION = Zap<EFBFBD>len<EFBFBD> motoru
|
|||
|
|
FlightEvent.Type.LIFTOFF = Vzl<EFBFBD>tnout
|
|||
|
|
FlightEvent.Type.LAUNCHROD = Vzd<EFBFBD>lenost vypou\u0161tec<65> tyce
|
|||
|
|
FlightEvent.Type.BURNOUT = Vyhoren<EFBFBD> motoru
|
|||
|
|
FlightEvent.Type.EJECTION_CHARGE = Ejection charge
|
|||
|
|
FlightEvent.Type.STAGE_SEPARATION = Oddelen<EFBFBD> stupne
|
|||
|
|
FlightEvent.Type.APOGEE = Vrchol
|
|||
|
|
FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Navr<EFBFBD>cen<EFBFBD> nasazen<65> zar<61>zen<65>
|
|||
|
|
FlightEvent.Type.GROUND_HIT = N<EFBFBD>raz do zeme
|
|||
|
|
FlightEvent.Type.SIMULATION_END = Konec simulace
|
|||
|
|
FlightEvent.Type.ALTITUDE = Zmena v<>\u0161ky
|
|||
|
|
|
|||
|
|
! ThrustCurveMotorColumns
|
|||
|
|
TCurveMotorCol.MANUFACTURER = V<EFBFBD>robce
|
|||
|
|
TCurveMotorCol.DESIGNATION = Pojmenov<EFBFBD>n<EFBFBD>
|
|||
|
|
TCurveMotorCol.TYPE = Druh
|
|||
|
|
TCurveMotorCol.DIAMETER = Prumer
|
|||
|
|
TCurveMotorCol.LENGTH = D<EFBFBD>lka
|
|||
|
|
|
|||
|
|
! RocketInfo
|
|||
|
|
RocketInfo.lengthLine.Length = D<EFBFBD>lka
|
|||
|
|
RocketInfo.lengthLine.maxdiameter = , max. prumer
|
|||
|
|
RocketInfo.massText1 = Hmotnost s motory
|
|||
|
|
RocketInfo.massText2 = Hmotnost bez motoru
|
|||
|
|
RocketInfo.at = v M=
|
|||
|
|
RocketInfo.cgText = Te\u017E<37>\u0161te:
|
|||
|
|
RocketInfo.cpText = Centrum tlaku:
|
|||
|
|
RocketInfo.stabText = Stabilita:
|
|||
|
|
RocketInfo.Warning = Varov<EFBFBD>n<EFBFBD>:
|
|||
|
|
RocketInfo.Calculating = Poc<EFBFBD>t<EFBFBD>m...
|
|||
|
|
RocketInfo.Apogee = Vrchol:
|
|||
|
|
RocketInfo.Maxvelocity = Max. rychlost:
|
|||
|
|
RocketInfo.Maxacceleration = Max. akcelerace:
|
|||
|
|
RocketInfo.apogeeValue = N/A
|
|||
|
|
RocketInfo.Mach = (Mach
|
|||
|
|
RocketInfo.velocityValue = N/A
|
|||
|
|
RocketInfo.accelerationValue = N/A
|
|||
|
|
|
|||
|
|
! FinSet
|
|||
|
|
FinSet.CrossSection.SQUARE = Ctvercov<EFBFBD>
|
|||
|
|
FinSet.CrossSection.ROUNDED = Obl<EFBFBD>
|
|||
|
|
FinSet.CrossSection.AIRFOIL = Aerodynamick<EFBFBD> profil
|
|||
|
|
FinSet.TabRelativePosition.FRONT = Tetiva u korene n<>be\u017En<45> hrany
|
|||
|
|
FinSet.TabRelativePosition.CENTER = Stred tetivy u korene
|
|||
|
|
FinSet.TabRelativePosition.END = Tetiva u korene odtokov<6F> hrany
|
|||
|
|
|
|||
|
|
! FlightDataType
|
|||
|
|
FlightDataType.TYPE_TIME = Cas
|
|||
|
|
FlightDataType.TYPE_ALTITUDE = Nadmorsk<EFBFBD> v<>\u0161ka
|
|||
|
|
FlightDataType.TYPE_VELOCITY_Z = Svisl<EFBFBD> rychlost
|
|||
|
|
FlightDataType.TYPE_ACCELERATION_Z = Svisl<EFBFBD> zrychlen<65>
|
|||
|
|
FlightDataType.TYPE_VELOCITY_TOTAL = Celkov<EFBFBD> rychlost
|
|||
|
|
FlightDataType.TYPE_ACCELERATION_TOTAL = Celkov<EFBFBD> zrychlen<65>
|
|||
|
|
FlightDataType.TYPE_POSITION_X = Pozice proti vetru
|
|||
|
|
FlightDataType.TYPE_POSITION_Y = Pozice po vetru
|
|||
|
|
FlightDataType.TYPE_POSITION_XY = Bocn<EFBFBD> vzd<7A>lenost
|
|||
|
|
FlightDataType.TYPE_POSITION_DIRECTION = Bocn<EFBFBD> smer
|
|||
|
|
FlightDataType.TYPE_VELOCITY_XY = Bocn<EFBFBD> rychlost
|
|||
|
|
FlightDataType.TYPE_ACCELERATION_XY = Bocn<EFBFBD> zrychlen<65>
|
|||
|
|
FlightDataType.TYPE_AOA = <EFBFBD>hel n<>behu
|
|||
|
|
FlightDataType.TYPE_ROLL_RATE = <EFBFBD>hlov<EFBFBD> rychlost klonen<65>
|
|||
|
|
FlightDataType.TYPE_PITCH_RATE = <EFBFBD>hlov<EFBFBD> rychlost klopen<65>
|
|||
|
|
FlightDataType.TYPE_YAW_RATE = <EFBFBD>hlov<EFBFBD> rychlost zat<61>cen<65>
|
|||
|
|
FlightDataType.TYPE_MASS = Hmotnost
|
|||
|
|
FlightDataType.TYPE_LONGITUDINAL_INERTIA = Pod<EFBFBD>ln<EFBFBD> moment setrvacnosti
|
|||
|
|
FlightDataType.TYPE_ROTATIONAL_INERTIA = Tociv<EFBFBD> moment setrvacnosti
|
|||
|
|
FlightDataType.TYPE_CP_LOCATION = Um<EFBFBD>sten<EFBFBD> pusobi\u0161te tlaku
|
|||
|
|
FlightDataType.TYPE_CG_LOCATION = Um<EFBFBD>sten<EFBFBD> te\u017Ei\u0161te
|
|||
|
|
FlightDataType.TYPE_STABILITY = Kvalita bezpecnosti stability
|
|||
|
|
FlightDataType.TYPE_MACH_NUMBER = Machovo c<>slo
|
|||
|
|
FlightDataType.TYPE_REYNOLDS_NUMBER = Reynoldsovo c<>slo
|
|||
|
|
FlightDataType.TYPE_THRUST_FORCE = Tah
|
|||
|
|
FlightDataType.TYPE_DRAG_FORCE = Brzd<EFBFBD>c<EFBFBD> s<>la
|
|||
|
|
FlightDataType.TYPE_DRAG_COEFF = Brzd<EFBFBD>c<EFBFBD> koeficient
|
|||
|
|
FlightDataType.TYPE_AXIAL_DRAG_COEFF = Osov<EFBFBD> brzd<7A>c<EFBFBD> koeficient
|
|||
|
|
FlightDataType.TYPE_FRICTION_DRAG_COEFF = Soucinitel brzdn<64>ho tren<65>
|
|||
|
|
FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Tlakov<EFBFBD> brzd<7A>c<EFBFBD> koeficient
|
|||
|
|
FlightDataType.TYPE_BASE_DRAG_COEFF = Z<EFBFBD>kladn<EFBFBD> brzd<7A>c<EFBFBD> koeficient
|
|||
|
|
FlightDataType.TYPE_NORMAL_FORCE_COEFF = Norm<EFBFBD>n<EFBFBD> silov<6F> koeficient
|
|||
|
|
FlightDataType.TYPE_PITCH_MOMENT_COEFF = Koeficient klopiv<69>ho momentu
|
|||
|
|
FlightDataType.TYPE_YAW_MOMENT_COEFF = Koeficient zat<61>civ<69>ho momentu
|
|||
|
|
FlightDataType.TYPE_SIDE_FORCE_COEFF = Koeficient bocn<63> s<>ly
|
|||
|
|
FlightDataType.TYPE_ROLL_MOMENT_COEFF = Koeficient kloniv<69>ho momentu
|
|||
|
|
FlightDataType.TYPE_ROLL_FORCING_COEFF = Koeficient kloniv<69> s<>ly
|
|||
|
|
FlightDataType.TYPE_ROLL_DAMPING_COEFF = Koeficinet kloniv<69>ho tlumen<65>
|
|||
|
|
FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Koeficient klopiv<69>ho tlumen<65>
|
|||
|
|
FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Koeficient zat<61>civ<69>ho tlumen<65>
|
|||
|
|
FlightDataType.TYPE_REFERENCE_LENGTH = Doporucen<EFBFBD> d<>lka
|
|||
|
|
FlightDataType.TYPE_REFERENCE_AREA = Doporucen<EFBFBD> obast
|
|||
|
|
FlightDataType.TYPE_ORIENTATION_THETA = Svisl<EFBFBD> orientace (zenit)
|
|||
|
|
FlightDataType.TYPE_ORIENTATION_PHI = Bocn<EFBFBD> orientace (azimut)
|
|||
|
|
FlightDataType.TYPE_WIND_VELOCITY = Rychlost vetru
|
|||
|
|
FlightDataType.TYPE_AIR_TEMPERATURE = Teplota vzduchu
|
|||
|
|
FlightDataType.TYPE_AIR_PRESSURE = Tlak vzduchu
|
|||
|
|
FlightDataType.TYPE_SPEED_OF_SOUND = Rychlost zvuku
|
|||
|
|
FlightDataType.TYPE_TIME_STEP = Simulacn<EFBFBD> krok
|
|||
|
|
FlightDataType.TYPE_COMPUTATION_TIME = V<EFBFBD>pocetn<EFBFBD> cas
|
|||
|
|
FlightDataType.TYPE_LATITUDE = Zemepisn<EFBFBD> \u0161<36>rka
|
|||
|
|
FlightDataType.TYPE_LONGITUDE = Zemepisn<EFBFBD> d<>lka
|
|||
|
|
FlightDataType.TYPE_CORIOLIS_ACCELERATION = Koriolisovo zrychlen<65>
|
|||
|
|
|
|||
|
|
! PlotConfiguration
|
|||
|
|
PlotConfiguration.Verticalmotion = Vertik<EFBFBD>ln<EFBFBD> pohyb vs. cas
|
|||
|
|
PlotConfiguration.Totalmotion = Celkov<EFBFBD> pohyb vs. cas
|
|||
|
|
PlotConfiguration.Flightside = Letov<EFBFBD> profil
|
|||
|
|
PlotConfiguration.Stability = Stabilita vs. cas
|
|||
|
|
PlotConfiguration.Dragcoef = Brzd<EFBFBD>c<EFBFBD> koeficient vs. Machovo c<>slo
|
|||
|
|
PlotConfiguration.Rollcharacteristics = Charakteristiky pr<70>cn<63>ho n<>klonu
|
|||
|
|
PlotConfiguration.Angleofattack = <EFBFBD>hel n<>behu a orientace
|
|||
|
|
vs cas
|
|||
|
|
PlotConfiguration.Simulationtime = Simulacn<EFBFBD> krok a v<>pocetn<74> cas
|
|||
|
|
|
|||
|
|
! Warning
|
|||
|
|
Warning.LargeAOA.str1 = Velk<EFBFBD> <20>hel n<>behu.
|
|||
|
|
Warning.LargeAOA.str2 = Velk<EFBFBD> <20>hel n<>behu (
|
|||
|
|
Warning.DISCONTINUITY = Nespojitost v prumeru tela rakety.
|
|||
|
|
Warning.THICK_FIN = Tlou\u0161tka stabiliz<69>toru se nemu\u017Ee modelovat presne.
|
|||
|
|
Warning.JAGGED_EDGED_FIN = Zubat<EFBFBD> hrany stabiliz<69>toru mohou b<>t vypocteny nepresne.
|
|||
|
|
Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
|
|||
|
|
Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Z<EFBFBD>chran<EFBFBD> zar<61>zen<65> se otevrelo, zat<61>mco motor st<73>le horel.
|
|||
|
|
Warning.FILE_INVALID_PARAMETER = Setk<EFBFBD>n<EFBFBD> s neplatn<74>m parametrem, ignorace.
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Scale dialog
|
|||
|
|
ScaleDialog.lbl.scaleRocket = Cel<EFBFBD> raketa
|
|||
|
|
ScaleDialog.lbl.scaleSubselection = Oznac a v\u0161echny subkomponenty
|
|||
|
|
ScaleDialog.lbl.scaleSelection = Pouze oznacen<65> komponenty
|
|||
|
|
ScaleDialog.title = Stupnice mer<65>tka
|
|||
|
|
ScaleDialog.lbl.scale = Mer<EFBFBD>tko:
|
|||
|
|
ScaleDialog.lbl.scale.ttip = Vyberte, zda chcete zmenit mer<65>tko cel<65>ho n<>vrhu nebo pouze vybran<61>ch souc<75>st<73>
|
|||
|
|
ScaleDialog.lbl.scaling = Uplatni zmenu mer<65>tka:
|
|||
|
|
ScaleDialog.lbl.scaling.ttip = V<EFBFBD>sledn<EFBFBD> velikost, hodnoty nad 100% znamenaj<61> zvet\u0161en<65> a hodnoty pod 100% zmen\u0161en<65> n<>vrhu.
|
|||
|
|
! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
|
|||
|
|
ScaleDialog.lbl.scaleFrom = Mer<EFBFBD>tko od
|
|||
|
|
ScaleDialog.lbl.scaleTo = do
|
|||
|
|
ScaleDialog.lbl.scaleFromTo.ttip = Definov<EFBFBD>n<EFBFBD> mer<65>tka na z<>klade puvodn<64> a v<>sledn<64> d<>lky.
|
|||
|
|
ScaleDialog.checkbox.scaleMass = Aktualizace vyj<79>dren<65> hodnoty hmotnosti
|
|||
|
|
ScaleDialog.checkbox.scaleMass.ttip = Mer<EFBFBD>tko hmotnosti komponenty a preps<70>n<EFBFBD> hodnoty hmotnosti tret<65> mocninou mer<65>tka
|
|||
|
|
ScaleDialog.button.scale = Mer<EFBFBD>tko
|
|||
|
|
ScaleDialog.undo.scaleRocket = Mer<EFBFBD>tko rakety
|
|||
|
|
ScaleDialog.undo.scaleComponent = Mer<EFBFBD>tko komponenty
|
|||
|
|
ScaleDialog.undo.scaleComponents = Mer<EFBFBD>tko komponent
|
|||
|
|
|
|||
|
|
!icons
|
|||
|
|
Icons.Undo = Zpet
|
|||
|
|
Icons.Redo = Znovu
|
|||
|
|
|
|||
|
|
OpenRocketPrintable.Partsdetail = Detail c<>st<73>
|
|||
|
|
OpenRocketPrintable.Fintemplates = \u0160ablony stabiliz<69>toru
|
|||
|
|
OpenRocketPrintable.Transitiontemplates = \u0160ablony prechodu
|
|||
|
|
OpenRocketPrintable.Noseconetemplates = \u0160ablony nosn<73>ho ku\u017Eele
|
|||
|
|
OpenRocketPrintable.Finmarkingguide = Oznacen<EFBFBD> pruvodce stabiliz<69>tory
|
|||
|
|
OpenRocketPrintable.DesignReport = Hl<EFBFBD>\u0161en<65> o n<>vrhu
|
|||
|
|
|
|||
|
|
OpenRocketDocument.Redo = Znovu
|
|||
|
|
OpenRocketDocument.Undo = Zpet
|
|||
|
|
|
|||
|
|
!EllipticalFinSet
|
|||
|
|
EllipticalFinSet.Ellipticalfinset = Eliptick<EFBFBD> soubor stabiliz<69>toru
|
|||
|
|
|
|||
|
|
! Optimization
|
|||
|
|
|
|||
|
|
! Modifiers
|
|||
|
|
|
|||
|
|
optimization.modifier.nosecone.length = D<EFBFBD>lka
|
|||
|
|
optimization.modifier.nosecone.length.desc = Optimalizace d<>lky celn<6C>ho ku\u017Eelu.
|
|||
|
|
optimization.modifier.nosecone.diameter = Prumer
|
|||
|
|
optimization.modifier.nosecone.diameter.desc = Optimalizace prumeru celn<6C>ho ku\u017Eelu.
|
|||
|
|
optimization.modifier.nosecone.thickness = Tlou\u0161tka
|
|||
|
|
optimization.modifier.nosecone.thickness.desc = Optimalizace tlou\u0161tky steny nosn<73>ho ku\u017Eelu.
|
|||
|
|
optimization.modifier.nosecone.shapeparameter = Parametry tvaru
|
|||
|
|
optimization.modifier.nosecone.shapeparameter.desc = Optimalizace parametru tvaru nosn<73>ho ku\u017Eelu.
|
|||
|
|
|
|||
|
|
optimization.modifier.transition.length = D<EFBFBD>lka
|
|||
|
|
optimization.modifier.transition.length.desc = Optimalizace d<>lky prechodu trupu.
|
|||
|
|
optimization.modifier.transition.forediameter = Pr<EFBFBD>dov<EFBFBD> prumer
|
|||
|
|
optimization.modifier.transition.forediameter.desc = Optimalizace pr<70>dov<6F>ho prumeru prechodu trupu.
|
|||
|
|
optimization.modifier.transition.aftdiameter = Z<EFBFBD>dov<EFBFBD> prumer
|
|||
|
|
optimization.modifier.transition.aftdiameter.desc = Optimalizace z<>dov<6F>ho prumeru prechodu trupu.
|
|||
|
|
optimization.modifier.transition.thickness = Tlou\u0161tka
|
|||
|
|
optimization.modifier.transition.thickness.desc = Optimalizace tlou\u0161tky steny prechodu trupu.
|
|||
|
|
optimization.modifier.transition.shapeparameter = Parametry tvaru
|
|||
|
|
optimization.modifier.transition.shapeparameter.desc = Optimalizace parametru tvaru prechodu trupu.
|
|||
|
|
|
|||
|
|
optimization.modifier.bodytube.length = D<EFBFBD>lka
|
|||
|
|
optimization.modifier.bodytube.length.desc = Optimalizace d<>lky telov<6F> trubky.
|
|||
|
|
optimization.modifier.bodytube.outerDiameter = Vnej\u0161<36> prumer
|
|||
|
|
optimization.modifier.bodytube.outerDiameter.desc = Optimalizace vnej\u0161<36>ho prumeru telov<6F> trubky pri zachov<6F>n<EFBFBD> tlou\u0161tky steny.
|
|||
|
|
optimization.modifier.bodytube.thickness = Tlou\u0161tka
|
|||
|
|
optimization.modifier.bodytube.thickness.desc = Optimalizace tlou\u0161tky steny telov<6F> trubky.
|
|||
|
|
|
|||
|
|
optimization.modifier.trapezoidfinset.rootChord = Tetiva u korene
|
|||
|
|
optimization.modifier.trapezoidfinset.rootChord.desc = Optimalizace tetivy u korene stabiliz<69>toru (d<>lka stabiliz<69>toru na tele rakety).
|
|||
|
|
optimization.modifier.trapezoidfinset.tipChord = Koncov<EFBFBD> tetiva
|
|||
|
|
optimization.modifier.trapezoidfinset.tipChord.desc = Optimalizace koncov<6F> tetivy stabiliz<69>toru (d<>lka stabiliz<69>toru na vnej\u0161<36>m okraji).
|
|||
|
|
optimization.modifier.trapezoidfinset.sweep = Ostr<EFBFBD> <20>hel
|
|||
|
|
optimization.modifier.trapezoidfinset.sweep.desc = Optimalizace ostr<74>ho <20>hlu stabiliz<69>toru (vzd<7A>lenost mezi n<>be\u017Enou hranou a kladn<64>m \u0161<36>pem).
|
|||
|
|
optimization.modifier.trapezoidfinset.height = V<EFBFBD>\u0161ka
|
|||
|
|
optimization.modifier.trapezoidfinset.height.desc = Optimalizace v<>\u0161ky (poloviny rozpet<65>) stabliz<69>toru.
|
|||
|
|
|
|||
|
|
optimization.modifier.ellipticalfinset.length = Tetiva u korene
|
|||
|
|
optimization.modifier.ellipticalfinset.length.desc = Optimalizace d<>lky tetivy u korene stabiliz<69>toru.
|
|||
|
|
optimization.modifier.ellipticalfinset.height = V<EFBFBD>\u0161ka
|
|||
|
|
optimization.modifier.ellipticalfinset.height.desc = Optimalizace v<>\u0161ky (poloviny rozpet<65>) stabiliz<69>toru.
|
|||
|
|
|
|||
|
|
optimization.modifier.finset.cant = <EFBFBD>hel n<>klonu
|
|||
|
|
optimization.modifier.finset.cant.desc = Optimalizace <20>hlu n<>klonu stabiliz<69>toru.
|
|||
|
|
optimization.modifier.finset.position = Pozice
|
|||
|
|
optimization.modifier.finset.position.desc = Optimalizace pozice stabiliz<69>toru pod<6F>l tela rakety.
|
|||
|
|
|
|||
|
|
optimization.modifier.launchlug.length = D<EFBFBD>lka
|
|||
|
|
optimization.modifier.launchlug.length.desc = Optimalizace d<>lky vypou\u0161tec<65>ho oka.
|
|||
|
|
optimization.modifier.launchlug.outerDiameter = Vnej\u0161<36> prumer
|
|||
|
|
optimization.modifier.launchlug.outerDiameter.desc = Optimalizace vnej\u0161<36>ho prumeru vypou\u0161tec<65>ho oka.
|
|||
|
|
optimization.modifier.launchlug.thickness = Tlou\u0161tka
|
|||
|
|
optimization.modifier.launchlug.thickness.desc = Optimalizace tlou\u0161tky vypou\u0161tec<65>ho oka pri zachov<6F>n<EFBFBD> konstantn<74>ho vnej\u0161<36>ho prumeru.
|
|||
|
|
optimization.modifier.launchlug.position = Pozice
|
|||
|
|
optimization.modifier.launchlug.position.desc = Optimalizce vypou\u0161tec<65>ho oka vzhledem k telu rakety.
|
|||
|
|
|
|||
|
|
|
|||
|
|
optimization.modifier.internalcomponent.position = Pozice
|
|||
|
|
optimization.modifier.internalcomponent.position.desc = Optimalizace pozice komponenty vzhledem rodicovsk<73> komponente.
|
|||
|
|
|
|||
|
|
optimization.modifier.masscomponent.mass = Hmotnost
|
|||
|
|
optimization.modifier.masscomponent.mass.desc = Optimalizace hmotnosti komponenty.
|
|||
|
|
|
|||
|
|
optimization.modifier.parachute.diameter = Prumer
|
|||
|
|
optimization.modifier.parachute.diameter.desc = Optimalizace prumeru vrchl<68>ku pad<61>ku.
|
|||
|
|
optimization.modifier.parachute.coefficient = Brzd<EFBFBD>c<EFBFBD> koeficient
|
|||
|
|
optimization.modifier.parachute.coefficient.desc = Optimalizace brzd<7A>c<EFBFBD>ho koeficientu pad<61>ku. Typick<63> pad<61>k m<> brzd<7A>c<EFBFBD> koeficient okolo 0.8.
|
|||
|
|
|
|||
|
|
optimization.modifier.streamer.length = D<EFBFBD>lka
|
|||
|
|
optimization.modifier.streamer.length.desc = Optimalizace d<>lky brzd<7A>c<EFBFBD>ho prou\u017Eku.
|
|||
|
|
optimization.modifier.streamer.width = \u0160<36>rka
|
|||
|
|
optimization.modifier.streamer.width.desc = Optimalizace \u0161<36>rky brzd<7A>c<EFBFBD>ho prou\u017Eku.
|
|||
|
|
optimization.modifier.streamer.aspectRatio = Pomer stran
|
|||
|
|
optimization.modifier.streamer.aspectRatio.desc = Optimalizace pomeru stran brzd<7A>c<EFBFBD>ho prou\u017Eku (d<>lka/\u0161<36>rka). NEMEL-by jste zvolit \u0161<36>rku nebo d<>lku brzd<7A>c<EFBFBD>ho prou\u017Eku ve stejn<6A>m pomeru.
|
|||
|
|
optimization.modifier.streamer.coefficient = Brzd<EFBFBD>c<EFBFBD> koeficient
|
|||
|
|
optimization.modifier.streamer.coefficient.desc = Optimalizace brzd<7A>c<EFBFBD>ho koeficinetu bryd<79>c<EFBFBD>ho prou\u017Eku.
|
|||
|
|
|
|||
|
|
optimization.modifier.recoverydevice.deployDelay = Zpo\u017Eden<65> otevren<65>
|
|||
|
|
optimization.modifier.recoverydevice.deployDelay.desc = Optimalizace zpo\u017Eden<65> otevren<65> n<>vratov<6F>ho zar<61>zen<65>.
|
|||
|
|
optimization.modifier.recoverydevice.deployAltitude = V<EFBFBD>\u0161ka otevren<65>
|
|||
|
|
optimization.modifier.recoverydevice.deployAltitude.desc = Optimalizace v<>\u0161ky otevren<65> n<>vratov<6F>ho zar<61>zen<65>.
|
|||
|
|
|
|||
|
|
optimization.modifier.rocketcomponent.overrideMass = Zmena hmotnosti
|
|||
|
|
optimization.modifier.rocketcomponent.overrideMass.desc = Optimalizace zmeny hmotnosti komponety.
|
|||
|
|
optimization.modifier.rocketcomponent.overrideCG = Zmena te\u017Ei\u0161te
|
|||
|
|
optimization.modifier.rocketcomponent.overrideCG.desc = Optimalizace zmeny te\u017Ei\u0161te komponenty.
|
|||
|
|
|
|||
|
|
optimization.modifier.motormount.overhang = Presah motoru
|
|||
|
|
optimization.modifier.motormount.overhang.desc = Optimalizace presahu motoru.
|
|||
|
|
optimization.modifier.motormount.delay = Zpo\u017Eden<65> zap<61>len<65> motoru
|
|||
|
|
optimization.modifier.motormount.delay.desc = Optimalizace zpo\u017Eden<65> zap<61>len<65> motoru.
|
|||
|
|
|
|||
|
|
|
|||
|
|
|
|||
|
|
|
|||
|
|
! General rocket design optimization dialog
|
|||
|
|
|
|||
|
|
GeneralOptimizationDialog.title = Optimalizace rakety
|
|||
|
|
GeneralOptimizationDialog.goal.maximize = Maximalizace hodnot
|
|||
|
|
GeneralOptimizationDialog.goal.minimize = Minimalizace hodnot
|
|||
|
|
GeneralOptimizationDialog.goal.seek = Hledej hodnotu
|
|||
|
|
GeneralOptimizationDialog.btn.start = Zac<EFBFBD>tek optimalizace
|
|||
|
|
GeneralOptimizationDialog.btn.stop = Konec optimalizace
|
|||
|
|
GeneralOptimizationDialog.lbl.paramsToOptimize = Parametry optimalizace:
|
|||
|
|
GeneralOptimizationDialog.btn.add = Pridej
|
|||
|
|
GeneralOptimizationDialog.btn.add.ttip = Pridej oznacen<65> parametry k optimalizaci
|
|||
|
|
GeneralOptimizationDialog.btn.remove = Odeber
|
|||
|
|
GeneralOptimizationDialog.btn.remove.ttip = Odeber oznacen<65> parametry z optimalizace
|
|||
|
|
GeneralOptimizationDialog.btn.removeAll = Odeber v\u0161e
|
|||
|
|
GeneralOptimizationDialog.btn.removeAll.ttip = Odeber v\u0161echny parametry z optimalizace
|
|||
|
|
GeneralOptimizationDialog.lbl.availableParams = Dostupn<EFBFBD> parametry:
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizationOpts = Nastaven<EFBFBD> optimalizace
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizeSim = Optimalizuj simulaci:
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizeSim.ttip = vyber kterou simulaci optimalizovat
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizeValue = Optimalizovan<EFBFBD> hodnota:
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizeValue.ttip = Vyber hodnota m<> b<>t optimalizov<6F>na
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizeGoal = Optimalizacn<EFBFBD> c<>l:
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Oznac c<>l optimalizace
|
|||
|
|
GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Vlastn<EFBFBD> hodota k hled<65>n<EFBFBD>
|
|||
|
|
GeneralOptimizationDialog.lbl.requireStability = Vy\u017Eadovan<61> stabilita
|
|||
|
|
GeneralOptimizationDialog.lbl.requireMinStability = Minim<EFBFBD>ln<EFBFBD> stabilita:
|
|||
|
|
GeneralOptimizationDialog.lbl.requireMinStability.ttip = Vy\u017Eadovan<61> minim<69>ln<6C> rozpet<65> statick<63> stability n<>vrhu
|
|||
|
|
GeneralOptimizationDialog.lbl.requireMaxStability = Maxim<EFBFBD>ln<EFBFBD> stabilita:
|
|||
|
|
GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Vy\u017Eadovan<61> maxim<69>ln<6C> rozpet<65> statick<63> stability n<>vrhu
|
|||
|
|
GeneralOptimizationDialog.status.bestValue = Nejlep\u0161<36> hodnota:
|
|||
|
|
GeneralOptimizationDialog.status.bestValue.ttip = Nejlep\u0161<36> optimalizacn<63> hodnota byla nalezena pr<70>li\u0161 daleko.
|
|||
|
|
GeneralOptimizationDialog.status.stepCount = Poc<EFBFBD>tac<EFBFBD> krok:
|
|||
|
|
GeneralOptimizationDialog.status.stepCount.ttip = Pocet kroku optimalizace, kter<65> bude vykon<6F>n.
|
|||
|
|
GeneralOptimizationDialog.status.evalCount = Ohodnocen<EFBFBD>:
|
|||
|
|
GeneralOptimizationDialog.status.evalCount.ttip = Celkov<EFBFBD> pocet funkcn<63>ch ohodnocen<65>(simulac<61>), kter<65> budou provedena.
|
|||
|
|
GeneralOptimizationDialog.status.stepSize = D<EFBFBD>lka kroku:
|
|||
|
|
GeneralOptimizationDialog.status.stepSize.ttip = Soucasn<EFBFBD> d<>lka optimalizacn<63>ho kroku (vzhledem k rozsahu optimalizacn<63>ch parametru)
|
|||
|
|
GeneralOptimizationDialog.btn.plotPath = Zakresli postup
|
|||
|
|
GeneralOptimizationDialog.btn.plotPath.ttip = Zakresli postup optimalizace (pouze jedno a dvoudimenzion<6F>ln<6C> optimalizace)
|
|||
|
|
GeneralOptimizationDialog.btn.save = Ulo\u017E postup
|
|||
|
|
GeneralOptimizationDialog.btn.save.ttip = Ulo\u017E v<>sledky funkcn<63>ch hodnocen<65> (simulac<61>) jako CSV soubor.
|
|||
|
|
GeneralOptimizationDialog.btn.apply = Aplikuj optimalizaci
|
|||
|
|
GeneralOptimizationDialog.btn.apply.ttip = Aplikuj optimalizacn<63> v<>sledky do n<>vrhu rakety
|
|||
|
|
GeneralOptimizationDialog.btn.reset = Reset
|
|||
|
|
GeneralOptimizationDialog.btn.reset.ttip = Resetovat raketov<6F> n<>vrh na aktu<74>ln<6C> konstrukci rakety
|
|||
|
|
GeneralOptimizationDialog.btn.close = Zavri
|
|||
|
|
GeneralOptimizationDialog.btn.close.ttip = Zavri dialog bez modifkov<6F>n<EFBFBD> n<>vrhu rakety
|
|||
|
|
GeneralOptimizationDialog.error.selectParams.text = Jako prvn<76> oznacte parametry k optimalizaci z dostupn<70>ch parametru.
|
|||
|
|
GeneralOptimizationDialog.error.selectParams.title = Oznac optimalizacn<63> parametry
|
|||
|
|
GeneralOptimizationDialog.error.optimizationFailure.text = Optimalizaci se nepodarilo spustit:
|
|||
|
|
GeneralOptimizationDialog.error.optimizationFailure.title = Optimalizace selhala
|
|||
|
|
GeneralOptimizationDialog.undoText = Pou\u017Eij optimalizaci
|
|||
|
|
GeneralOptimizationDialog.basicSimulationName = Z<EFBFBD>kladn<EFBFBD> simulace
|
|||
|
|
GeneralOptimizationDialog.noSimulationName = Bez simulace
|
|||
|
|
GeneralOptimizationDialog.table.col.parameter = Parametery
|
|||
|
|
GeneralOptimizationDialog.table.col.current = Soucasn<EFBFBD>
|
|||
|
|
GeneralOptimizationDialog.table.col.min = Minimum
|
|||
|
|
GeneralOptimizationDialog.table.col.max = Maximum
|
|||
|
|
GeneralOptimizationDialog.export.header = Vlo\u017E hlavicku
|
|||
|
|
GeneralOptimizationDialog.export.header.ttip = Vlo\u017E hlavicku jako prvn<76> r<>dek obsahuj<75>c<EFBFBD> popis pusobnosti.
|
|||
|
|
GeneralOptimizationDialog.export.stability = Stabilita
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Dialog for plotting optimization results
|
|||
|
|
OptimizationPlotDialog.title = V<EFBFBD>sledky optimalizace
|
|||
|
|
OptimizationPlotDialog.lbl.zoomInstructions = Kliknout a t<>hnout dolu+doprava k pribl<62>\u017Een<65>, dolu+doleva k odd<64>len<65>
|
|||
|
|
OptimizationPlotDialog.plot1d.title = V<EFBFBD>sledky optimalizace
|
|||
|
|
OptimizationPlotDialog.plot1d.series = V<EFBFBD>sledky optimalizace
|
|||
|
|
OptimizationPlotDialog.plot2d.title = Cestak k optimalizaci
|
|||
|
|
OptimizationPlotDialog.plot2d.path = Cestak k optimalizaci
|
|||
|
|
OptimizationPlotDialog.plot2d.evals = Ohodnocen<EFBFBD>
|
|||
|
|
OptimizationPlotDialog.plot.ttip.stability = Stabilita:
|
|||
|
|
OptimizationPlotDialog.plot.label.optimum = Optimum
|
|||
|
|
|
|||
|
|
! Optimization parameters
|
|||
|
|
MaximumAltitudeParameter.name = Nejvz\u0161\u0161<36> nadmorsk<73> v<>\u0161ka
|
|||
|
|
MaximumVelocityParameter.name = Maxim<EFBFBD>ln<EFBFBD> rychlost
|
|||
|
|
MaximumAccelerationParameter.name = Maxim<EFBFBD>ln<EFBFBD> akcelerace
|
|||
|
|
StabilityParameter.name = Stabilita
|
|||
|
|
GroundHitVelocityParameter.name = Rychlost n<>razu na zem
|
|||
|
|
LandingDistanceParameter.name = Prist<EFBFBD>vac<EFBFBD> vzd<7A>lenost
|
|||
|
|
TotalFlightTimeParameter.name = Celkov<EFBFBD> letov<6F> cas
|
|||
|
|
DeploymentVelocityParameter.name = Rychlost pri rozbalen<65> pad<61>ku
|
|||
|
|
|
|||
|
|
|
|||
|
|
! Compass directions drawn on a compass rose.
|
|||
|
|
CompassRose.lbl.north = S
|
|||
|
|
CompassRose.lbl.east = V
|
|||
|
|
CompassRose.lbl.south = J
|
|||
|
|
CompassRose.lbl.west = Z
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! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
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CompassSelectionButton.lbl.N = S
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CompassSelectionButton.lbl.NE = SV
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CompassSelectionButton.lbl.E = V
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CompassSelectionButton.lbl.SE = JV
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CompassSelectionButton.lbl.S = J
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CompassSelectionButton.lbl.SW = JZ
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CompassSelectionButton.lbl.W = Z
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CompassSelectionButton.lbl.NW = SZ
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SlideShowDialog.btn.next = Dal\u0161<36>
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SlideShowDialog.btn.prev = Predchoz<EFBFBD>
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SlideShowLinkListener.error.title = Prohl<EFBFBD>dka programu nebyla nalezena
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SlideShowLinkListener.error.msg = Prominte, vybran<61> prohl<68>dka nebyla je\u0161te naps<70>na.
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GuidedTourSelectionDialog.title = Prohl<EFBFBD>dky programu
|
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GuidedTourSelectionDialog.lbl.selectTour = Vyberte prohl<68>dku programu:
|
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GuidedTourSelectionDialog.lbl.description = Popis prohl<68>dkz:
|
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GuidedTourSelectionDialog.lbl.length = Pocet sl<73>du:
|
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GuidedTourSelectionDialog.btn.start = Zacni prohl<68>dku!
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! Custom Fin BMP Importer
|
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CustomFinImport.button.label = Importuj z BMP
|
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CustomFinImport.filter = Bitmapov<EFBFBD> soubory (*.bmp)
|
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CustomFinImport.badFinImage = Nevalidn<EFBFBD> obr<62>zek stabiliz<69>toru. Obr<62>zek mus<75> b<>t cern<72> a b<>l<EFBFBD> (cern<72> pro stabiliz<69>tor), nesm<73> se dot<6F>kat z<>dn<64> strany, krome spodku obr<62>zku, kter<65> je podstavou stabiliz<69>toru.
|
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CustomFinImport.errorLoadingFile = Chyba behem nahr<68>v<EFBFBD>n<EFBFBD> souboru:
|
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CustomFinImport.errorParsingFile = Chyba behem zpracov<6F>v<EFBFBD>n<EFBFBD> obr<62>zku stabiliz<69>toru:
|
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CustomFinImport.undo = Importovat sadu volno tvarov<6F>ch stabiliz<69>toru
|
|||
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CustomFinImport.error.title = Chyba behem nahr<68>v<EFBFBD>n<EFBFBD> profilu stabiliz<69>toru
|
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CustomFinImport.error.badimage = Nemohu vyvodit tvar stabiliz<69>toru z obr<62>zku.
|
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