c3cfb2e781
Added l10n message keys for new column in SimulationPanel. Added function MathUtil.interpolate which does linear interpolation of intermediate values. This is used in FlightData for computing Velocity at deployment and Velocity at launch rod clearance.
43 lines
1.8 KiB
Plaintext
43 lines
1.8 KiB
Plaintext
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The current OpenRocket file format is "documented" only as the
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reference implementation. This will hopefully change in the future.
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The "version" attribute of the <openrocket> tag describes the file
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format version used, while the "creator" attribute MAY describe the
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software version used to write the document.
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The file format version is increased every time the format is
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changed. The minor number is increased when changes are made that are
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mostly backward-compatible, meaning that older software versions
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should be able to read the design sans the new features. The major
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number is increased when changes are made that render the design
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problematic or impossible to read for older software. For maximum
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compatibility software should save a file in the oldest file format
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version that supports all the necessary design features.
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The following file format versions exist:
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0.9: Used before the first public release of Openrocket; effectively
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equivalent to 1.0. Should not be used when writing documents.
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OpenRocket accepts this version when reading files, but other
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software need not.
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1.0: File format version of the first public release (OpenRocket 0.9.0)
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1.1: Introduced with OpenRocket 0.9.4. Adds support for saving fin
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tabs (<tabheight>, <tablength> and <tabposition> elements) and
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allows attaching subcomponents to a tube coupler (previously
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forbidden).
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1.2: Introduced with OpenRocket 1.1.1. Adds the <digest> tag to
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motor definitions. The digest uniquely identifies the
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functional characteristics of a particular thrust curve motor.
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1.3: Introduced with OpenRocket 1.1.9. Adds the <launchlongitude> and
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<geodeticmethod> parameters to the simulation conditions element.
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1.4: Introduced with OpenRocket 1.1.10. Adds the launchrodvelocity and
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deploymentvelocity attributes to <flightdata> element. |