version 1.1.9
This commit is contained in:
Sampo Niskanen
parent
d82a370dd4
commit
ab9bf0bce3
10
ChangeLog
10
ChangeLog
@ -1,6 +1,14 @@
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2011-11-24 Sampo Niskanen
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* Released version 1.1.9
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2011-11-18 Doug Pedrick
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* Printable Fin Marking Guides, Transitions, and Nose Cones (simple projection only)
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* Printable Fin Marking Guides, Transitions, and Nose Cones
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2011-10-20 Sampo Niskanen
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* [BUG] NPE if plot data type is not present
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2011-10-11 Sampo Niskanen
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@ -2,7 +2,7 @@
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OpenRocket - an Open Source model rocket simulator
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--------------------------------------------------
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Copyright (C) 2007-2010 Sampo Niskanen
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Copyright (C) 2007-2011 Sampo Niskanen
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For license information see the file LICENSE.TXT.
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@ -25,5 +25,8 @@ Contributions have been made by:
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--------------------------------
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Sampo Niskanen, main developer
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Doug Pedrick, support for reading RockSim designs
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Doug Pedrick, support for reading RockSim designs, printing
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Richard Graham, geodetic computations
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Boris du Reau, internationalization
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Tripoli France, Tripoli Spain, Stefan Lobas / ERIG, translations
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10
ReleaseNotes
10
ReleaseNotes
@ -1,3 +1,13 @@
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OpenRocket 1.1.9 (2011-11-24):
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-------------------------------
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This release calculates rocket flight in real-world coordinates and
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takes into account geodetic effects (including coriolis effect) thanks
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to work by Richard Graham. Printing of transitions, nose cone
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profiles and fin marking guides is available thanks to Doug Pedrick.
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It also contains some usability features and bug fixes.
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OpenRocket 1.1.8 (2011-08-25):
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-------------------------------
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@ -1,7 +1,7 @@
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# The OpenRocket build version
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build.version=1.1.9pre
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build.version=1.1.9
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# The source of the package. When building a package for a specific
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@ -30,7 +30,8 @@ public class AboutDialog extends JDialog {
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"<font size=\"+1\"><b>OpenRocket has been developed by:</b></font><br><br>" +
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"Sampo Niskanen (main developer)<br>" +
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"Doug Pedrick (RockSim file format, printing)<br>" +
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"Boris du Reau (internationalization, translation lead)<br><br>" +
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"Boris du Reau (internationalization, translation lead)<br>" +
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"Richard Graham (geodetic computations)<br><br>" +
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"<b>Translations by:</b><br><br>" +
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"Tripoli France (French)<br>" +
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"Stefan Lobas / ERIG e.V. (German)<br>" +
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@ -88,8 +88,6 @@ public class SimulationEditDialog extends JDialog {
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private static final Translator trans = Application.getTranslator();
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// FIXME: NPE if FlightDataType has disappeared
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public SimulationEditDialog(Window parent, Simulation s) {
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this(parent, s, 0);
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}
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@ -123,7 +123,7 @@ public class SimulationRunDialog extends JDialog {
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//// Simulation time:
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panel.add(new JLabel(trans.get("SimuRunDlg.lbl.Simutime") + " "), "gapright para");
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timeLabel = new JLabel("");
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panel.add(timeLabel, "growx, wrap rel");
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panel.add(timeLabel, "growx, wmin 200lp, wrap rel");
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//// Altitude:
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panel.add(new JLabel(trans.get("SimuRunDlg.lbl.Altitude") + " "));
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@ -118,8 +118,6 @@ public class SimulationPlotPanel extends JPanel {
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}
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}
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// FIXME: Bugs when expected branch is not present
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configurationSelector.addItemListener(new ItemListener() {
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@Override
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public void itemStateChanged(ItemEvent e) {
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@ -189,7 +187,7 @@ public class SimulationPlotPanel extends JPanel {
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typeSelectorPanel = new JPanel(new MigLayout("gapy rel"));
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JScrollPane scroll = new JScrollPane(typeSelectorPanel);
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this.add(scroll, "spany 2, height 10px, grow 100, gapright para");
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this.add(scroll, "spany 2, height 10px, wmin 400lp, grow 100, gapright para");
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//// Flight events
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@ -379,10 +377,6 @@ public class SimulationPlotPanel extends JPanel {
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private JComboBox axisSelector;
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public PlotTypeSelector(int index, FlightDataType type) {
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this(index, type, null, -1);
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}
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public PlotTypeSelector(int plotIndex, FlightDataType type, Unit unit, int position) {
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super(new MigLayout("ins 0"));
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@ -6,9 +6,6 @@ package net.sf.openrocket.gui.print;
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import java.awt.Graphics2D;
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import java.io.IOException;
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import java.text.DecimalFormat;
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import java.util.ArrayList;
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import java.util.Iterator;
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import java.util.List;
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import net.sf.openrocket.document.OpenRocketDocument;
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import net.sf.openrocket.document.Simulation;
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@ -152,7 +149,7 @@ public class DesignReport {
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PrintUtilities.addText(document, PrintUtilities.BIG_BOLD, ROCKET_DESIGN);
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Rocket rocket = rocketDocument.getRocket();
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final Configuration configuration = rocket.getDefaultConfiguration();
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final Configuration configuration = rocket.getDefaultConfiguration().clone();
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configuration.setAllStages();
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PdfContentByte canvas = writer.getDirectContent();
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@ -219,8 +216,6 @@ public class DesignReport {
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String[] motorIds = rocket.getMotorConfigurationIDs();
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List<Double> stageMasses = getStageMasses(rocket);
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for (int j = 0; j < motorIds.length; j++) {
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String motorId = motorIds[j];
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if (motorId != null) {
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@ -244,29 +239,6 @@ public class DesignReport {
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}
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}
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/**
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* Get the motor list for all motor mounts.
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*
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* @param theRocket the rocket object
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* @param theMid the motor id
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*
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* @return a list of Motor
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*/
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private List<Motor> getMotorList(final Rocket theRocket, final String theMid) {
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Iterator<RocketComponent> components = theRocket.iterator();
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final List<Motor> motorList = new ArrayList<Motor>();
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while (components.hasNext()) {
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RocketComponent rocketComponent = components.next();
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if (rocketComponent instanceof MotorMount) {
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MotorMount mm = (MotorMount) rocketComponent;
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final Motor motor = mm.getMotor(theMid);
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if (motor != null) {
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motorList.add(motor);
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}
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}
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}
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return motorList;
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}
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/**
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* Paint a diagram of the rocket into the PDF document.
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@ -545,27 +517,4 @@ public class DesignReport {
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return target.replace("]", "");
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}
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/**
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* Return a list of cumulative stage masses. The latter masses include the mass
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* of the upper stages as well.
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*
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* @param rocket the rocket
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* @return a list containing the cumulative stage masses
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*/
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private List<Double> getStageMasses(final Rocket rocket) {
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List<Double> masses = new ArrayList<Double>();
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int stages = rocket.getStageCount();
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Configuration config = new Configuration(rocket);
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MassCalculator calc = new BasicMassCalculator();
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for (int i = 0; i < stages; i++) {
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config.setToStage(i);
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masses.add(calc.getCG(config, MassCalcType.NO_MOTORS).weight);
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}
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return masses;
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}
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}
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@ -21,6 +21,7 @@ public class PrintFigure extends RocketFigure {
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super(configuration);
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}
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@Override
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protected double computeTy(int heightPx) {
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super.computeTy(heightPx);
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return 0;
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@ -4,7 +4,11 @@
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*/
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package net.sf.openrocket.gui.print;
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import java.util.*;
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import java.util.Iterator;
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import java.util.Map;
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import java.util.Set;
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import java.util.TreeMap;
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import java.util.TreeSet;
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/**
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* Instances of this class are meant to keep track of what the user has selected to be printed.
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@ -67,6 +71,7 @@ public class PrintableContext implements Comparable<PrintableContext>, Iterable<
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}
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/** PrintableContext iterator. */
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@Override
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public Iterator<PrintableContext> iterator() {
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return new Iterator<PrintableContext>() {
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@ -1,12 +1,14 @@
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package net.sf.openrocket.gui.print;
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import java.awt.Graphics2D;
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import java.awt.Rectangle;
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import java.awt.Shape;
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import net.sf.openrocket.gui.rocketfigure.TransitionShapes;
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import net.sf.openrocket.rocketcomponent.NoseCone;
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import net.sf.openrocket.rocketcomponent.Transition;
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import net.sf.openrocket.util.Transformation;
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import java.awt.*;
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public class PrintableNoseCone extends AbstractPrintableTransition {
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/**
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@ -40,6 +42,7 @@ public class PrintableNoseCone extends AbstractPrintableTransition {
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*
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* @param g2 the graphics context
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*/
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@Override
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protected void draw(Graphics2D g2) {
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Shape[] shapes = TransitionShapes.getShapesSide(target, Transformation.rotate_x(0d), PrintUnit.METERS.toPoints(1));
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@ -1,14 +1,15 @@
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package net.sf.openrocket.gui.print;
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import net.sf.openrocket.rocketcomponent.Transition;
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import java.awt.*;
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import java.awt.BasicStroke;
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import java.awt.Graphics2D;
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import java.awt.geom.Arc2D;
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import java.awt.geom.GeneralPath;
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import java.awt.geom.Line2D;
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import java.awt.geom.Path2D;
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import java.awt.geom.Point2D;
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import net.sf.openrocket.rocketcomponent.Transition;
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/**
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* This class allows for a Transition to be printable. It does so by decorating an existing transition (which will not be
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* modified) and rendering it within a JPanel. The JPanel is not actually visualized on a display, but instead renders
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@ -184,6 +185,7 @@ public class PrintableTransition extends AbstractPrintableTransition {
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*
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* @param g2 the graphics context
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*/
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@Override
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protected void draw(Graphics2D g2) {
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//Render it.
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g2.draw(gp);
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@ -109,7 +109,6 @@ public class RocketPanel extends JPanel implements TreeSelectionListener, Change
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private SimulationWorker backgroundSimulationWorker = null;
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private boolean dirty = false;
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private List<ChangeListener> listeners = new ArrayList<ChangeListener>();
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@ -1,18 +1,18 @@
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package net.sf.openrocket.models.gravity;
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//import net.sf.openrocket.util.Monitorable;
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import net.sf.openrocket.util.Monitorable;
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import net.sf.openrocket.util.WorldCoordinate;
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/**
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* An interface to modelling gravitational acceleration.
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* An interface for modeling gravitational acceleration.
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*
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* @author Sampo Niskanen <sampo.niskanen@iki.fi>
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*/
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public interface GravityModel extends Monitorable {
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/**
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* Compute the gravity at a given world coordinate
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* Compute the gravitational acceleration at a given world coordinate
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*
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* @param wc the world coordinate location
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* @return gravitational acceleration in m/s/s
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*/
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@ -4,7 +4,7 @@ import net.sf.openrocket.util.MathUtil;
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import net.sf.openrocket.util.WorldCoordinate;
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/**
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* A gravity model based on the WGS84 elipsoid.
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* A gravity model based on the WGS84 ellipsoid.
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*
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* @author Richard Graham <richard@rdg.cc>
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*/
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@ -44,7 +44,7 @@ public class WGSGravityModel implements GravityModel {
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// Apply correction due to altitude. Note this assumes a spherical earth, but it is a small correction
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// so it probably doesn't really matter. Also does not take into account gravity of the atmosphere, again
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// correction could be done but not really necessary.
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double g_alt = g_0 * Math.pow(WorldCoordinate.REARTH / (WorldCoordinate.REARTH + wc.getAltitude()), 2);
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double g_alt = g_0 * MathUtil.pow2(WorldCoordinate.REARTH / (WorldCoordinate.REARTH + wc.getAltitude()));
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return g_alt;
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}
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@ -93,8 +93,6 @@ public abstract class AbstractSimulationStepper implements SimulationStepper {
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}
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// Compute conditions
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//double altitude = status.getRocketPosition().z + status.getSimulationConditions().getLaunchAltitude();
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//gravity = status.getSimulationConditions().getGravityModel().getGravity(altitude);
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gravity = status.getSimulationConditions().getGravityModel().getGravity(status.getRocketWorldPosition());
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// Call post-listener
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@ -54,7 +54,7 @@ public enum GeodeticComputationStrategy {
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double newAlt = location.getAltitude() + delta.z;
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// bearing (in radians, clockwise from north);
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// d/R is the angular distance (in radians), where d is the distance traveled and R is the earth’s radius
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// d/R is the angular distance (in radians), where d is the distance traveled and R is the earth's radius
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double d = MathUtil.hypot(delta.x, delta.y);
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// Check for zero movement before computing bearing
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@ -99,7 +99,7 @@ public enum GeodeticComputationStrategy {
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double newAlt = location.getAltitude() + delta.z;
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// bearing (in radians, clockwise from north);
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// d/R is the angular distance (in radians), where d is the distance traveled and R is the earth’s radius
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// d/R is the angular distance (in radians), where d is the distance traveled and R is the earth's radius
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double d = MathUtil.hypot(delta.x, delta.y);
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// Check for zero movement before computing bearing
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@ -25,10 +25,6 @@ public enum LineStyle {
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DASHDOT("LineStyle.Dash-dotted", new float[] { 8f, 3f, 2f, 3f });
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private static final Translator trans = Application.getTranslator();
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static {
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System.out.println("*** LineStyle initialized trans:" + trans + " ***");
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System.err.println("*** LineStyle initialized ***");
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}
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private final String name;
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private final float[] dashes;
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@ -0,0 +1,42 @@
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package net.sf.openrocket.models.gravity;
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import static org.junit.Assert.assertEquals;
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import net.sf.openrocket.util.WorldCoordinate;
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import org.junit.Test;
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public class WGSGravityModelTest {
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private WGSGravityModel model = new WGSGravityModel();
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@Test
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public void testSurfaceGravity() {
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// Equator
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test(0, 0, 0, 9.780);
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// Mid-latitude
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test(45, 0, 0, 9.806);
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// Mid-latitude
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test(45, 99, 0, 9.806);
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// South pole
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test(-90, 0, 0, 9.832);
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}
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@Test
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public void testAltitudeEffect() {
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test(45, 0, -100, 9.806);
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test(45, 0, 0, 9.806);
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test(45, 0, 10, 9.806);
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test(45, 0, 100, 9.806);
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test(45, 0, 1000, 9.803);
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test(45, 0, 10000, 9.775);
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test(45, 0, 100000, 9.505);
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}
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private void test(double lat, double lon, double alt, double g) {
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WorldCoordinate wc = new WorldCoordinate(lat, lon, alt);
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assertEquals(g, model.getGravity(wc), 0.001);
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assertEquals(g, model.getGravity(wc), 0.001);
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}
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}
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@ -45,6 +45,7 @@ public class GeodeticComputationStrategyTest {
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// Test zero movement
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System.out.println("\nTesting zero movement");
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testAddCoordinate(50.0, 20.0, 0, 123, 50.0, 20.0, false);
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@ -55,22 +56,27 @@ public class GeodeticComputationStrategyTest {
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// Long distance NE over England, crosses Greenwich meridian
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// 50 03N 005 42W to 58 38N 003 04E is 1109km at 027 16'07"
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System.out.println("\nTesting 1109km NE over England");
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testAddCoordinate(50 + 3 * min, -5 - 42 * min, 1109000, 27 + 16 * min + 7 * sec, 58 + 38 * min, 3 + 4 * min, false);
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// SW over Brazil
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// -10N -60E to -11N -61E is 155.9km at 224 25'34"
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System.out.println("\nTesting 155km SW over Brazil");
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testAddCoordinate(-10, -60, 155900, 224 + 25 * min + 34 * sec, -11, -61, true);
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// NW over the 180 meridian
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// 63N -179E to 63 01N 179E is 100.9km at 271 56'34"
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System.out.println("\nTesting 100km NW over 180 meridian");
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testAddCoordinate(63, -179, 100900, 271 + 56 * min + 34 * sec, 63 + 1 * min, 179, true);
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// NE near the north pole
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// 89 50N 0E to 89 45N 175E is 46.29 km at 003 00'01"
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System.out.println("\nTesting 46km NE near north pole");
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testAddCoordinate(89 + 50 * min, 0, 46290, 3 + 0 * min + 1 * sec, 89 + 45 * min, 175, false);
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// S directly over south pole
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// -89 50N 12E to -89 45N 192E is 46.33km at 180 00'00"
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System.out.println("\nTesting 46km directly over south pole ");
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testAddCoordinate(-89 - 50 * min, 12, 46330, 180, -89 - 45 * min, -168, false);
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}
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@ -103,20 +109,20 @@ public class GeodeticComputationStrategyTest {
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// Test WGS84
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/*
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* TODO: Since the example values are computed using a spherical earth approximation,
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||||
* the WGS84 method will have significantly larger errors. The tolerance should be
|
||||
* increased correspondingly.
|
||||
* Note: Since the example values are computed using a spherical earth approximation,
|
||||
* the WGS84 method will have significantly larger errors. A tolerance of 1% accommodates
|
||||
* all cases except the NE flight near the north pole, where the ellipsoidal effect is
|
||||
* the greatest.
|
||||
*/
|
||||
//tolerance = ...
|
||||
tolerance = 0.04 * distance / 111325;
|
||||
System.out.println("\nWGS84 tolerance: " + tolerance);
|
||||
result = GeodeticComputationStrategy.WGS84.addCoordinate(result, coord);
|
||||
result = GeodeticComputationStrategy.WGS84.addCoordinate(wc, coord);
|
||||
|
||||
System.out.println("Difference Lat: " + Math.abs(finalLatitude - result.getLatitudeDeg()));
|
||||
System.out.println("Difference Lon: " + Math.abs(finalLongitude - result.getLongitudeDeg()));
|
||||
// FIXME: Re-enable these when they function
|
||||
// assertEquals(finalLatitude, result.getLatitudeDeg(), tolerance);
|
||||
// assertEquals(finalLongitude, result.getLongitudeDeg(), tolerance);
|
||||
// assertEquals(1000.0, result.getAltitude(), 0.0);
|
||||
assertEquals(finalLatitude, result.getLatitudeDeg(), tolerance);
|
||||
assertEquals(finalLongitude, result.getLongitudeDeg(), tolerance);
|
||||
assertEquals(1000.0, result.getAltitude(), 0.0);
|
||||
|
||||
|
||||
// Test FLAT
|
||||
|
||||
@ -80,21 +80,33 @@ header("Content-type: text/plain");
|
||||
$version = $_GET["version"];
|
||||
$updates = "";
|
||||
|
||||
$unstable = "1.1.8";
|
||||
$unstable = "1.1.9";
|
||||
$stable = "1.0.0";
|
||||
|
||||
if (preg_match("/^1\.1\.7/", $version)) {
|
||||
if (preg_match("/^1\.1\.8/", $version)) {
|
||||
$updates = "Version: " . $unstable . "\n" .
|
||||
"6: Additional template printing\n" .
|
||||
"5: Geodetic computations\n" .
|
||||
"4: Bug fixes\n" .
|
||||
"";
|
||||
} else if (preg_match("/^1\.1\.7/", $version)) {
|
||||
$updates = "Version: " . $unstable . "\n" .
|
||||
"6: Additional template printing\n" .
|
||||
"5: Geodetic computations\n" .
|
||||
"4: Bug fixes\n" .
|
||||
"";
|
||||
} else if (preg_match("/^1\.1\.6/", $version)) {
|
||||
$updates = "Version: " . $unstable . "\n" .
|
||||
"8: Automatic rocket design optimization\n" .
|
||||
"6: Additional template printing\n" .
|
||||
"5: Geodetic computations\n" .
|
||||
"";
|
||||
} else if (preg_match("/^1\.1\.5/", $version)) {
|
||||
$updates = "Version: " . $unstable . "\n" .
|
||||
"8: Automatic rocket design optimization\n" .
|
||||
"6: Initial localization support\n" .
|
||||
"6: Additional template printing\n" .
|
||||
"5: Geodetic computations\n" .
|
||||
"5: Scaling support\n" .
|
||||
"4: Bug fixes\n" .
|
||||
"";
|
||||
|
||||
@ -48,6 +48,18 @@
|
||||
<div class="content">
|
||||
<div class="news">
|
||||
<h2>Recent news:</h2>
|
||||
<p><span class="date">24.11.2011:</span> Version 1.1.9 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
<p>For this version Richard Graham has implemented geodetic
|
||||
computation methods, which take into account the curvature of the
|
||||
Earth and the coriolis effect. The computation method is selected
|
||||
by the <em>Geodetic calculations</em> option in the simulation
|
||||
options. It's not <em>(yet)</em> a full spherical computation model, but
|
||||
should be accurate enough for almost all sub-orbital needs.</p>
|
||||
<p>Doug Pedrick has also enhanced the printing system with the
|
||||
ability to print fin positioning guides, transition templates and
|
||||
nose cone profiles. Other smaller enhancements and bug fixes are
|
||||
also included.</p>
|
||||
<p><span class="date">25.8.2011:</span> Version 1.1.8 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
<p>This release contains bug fixes to the optimization methods.
|
||||
@ -66,16 +78,6 @@
|
||||
easy to optimize against particulars of the simulation methods,
|
||||
instead of true physical phenomena. Always keep common sense at
|
||||
hand and take the results with a grain of salt.</p>
|
||||
<p><span class="date">22.7.2011:</span> Version 1.1.6 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
<p>This release includes initial localization support and
|
||||
translations to French, German and Spanish. This is thanks to the
|
||||
great work of Boris du Reau, and the teams from Tripoli France,
|
||||
Tripoli Spain and ERIG e.V. If you prefer to use some other
|
||||
language than the system default, you can select the language on
|
||||
the "Options" tab of the preferences dialog.</p>
|
||||
<p>The release also includes design scaling support and numerous bug
|
||||
fixes.</p>
|
||||
</div>
|
||||
<div class="contentholder">
|
||||
<h2>Ready packages</h2>
|
||||
@ -94,13 +96,13 @@
|
||||
<a href="http://sourceforge.net/donate/index.php?group_id=260357"><img src="project-support.jpg" width="88" height="32" alt="Support This Project" /></a>
|
||||
</div>
|
||||
<div class="downloadbox">
|
||||
<a class="main" href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.8/OpenRocket-1.1.8.jar/download">
|
||||
<a class="main" href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.9/OpenRocket-1.1.9.jar/download">
|
||||
<strong>Download now!</strong>
|
||||
<span>OpenRocket-1.1.8.jar</span>
|
||||
<span>OpenRocket-1.1.9.jar</span>
|
||||
</a>
|
||||
<span class="alternative">
|
||||
<a href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.8/ReleaseNotes/view">Release notes</a> |
|
||||
<a href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.8/OpenRocket-1.1.8-src.zip/download">Source code</a>
|
||||
<a href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.9/ReleaseNotes/view">Release notes</a> |
|
||||
<a href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.9/OpenRocket-1.1.9-src.zip/download">Source code</a>
|
||||
</span>
|
||||
</div>
|
||||
<h3>Stable release</h3>
|
||||
@ -117,7 +119,7 @@
|
||||
Windows) by double-clicking the package icon. No installation is
|
||||
required.</p>
|
||||
<p>From the command line OpenRocket can be started by
|
||||
<span class="command">java -jar OpenRocket-1.1.8.jar</span></p>
|
||||
<span class="command">java -jar OpenRocket-1.1.9.jar</span></p>
|
||||
|
||||
</div>
|
||||
<div class="clear"></div>
|
||||
|
||||
@ -49,12 +49,12 @@
|
||||
<h2>Introduction</h2>
|
||||
<div class="rightpane">
|
||||
<div class="downloadbox">
|
||||
<a class="main" href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.8/OpenRocket-1.1.8.jar/download">
|
||||
<a class="main" href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.9/OpenRocket-1.1.9.jar/download">
|
||||
<strong>Download now!</strong>
|
||||
<span>OpenRocket-1.1.8.jar</span>
|
||||
<span>OpenRocket-1.1.9.jar</span>
|
||||
</a>
|
||||
<span class="alternative">
|
||||
<a href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.8/ReleaseNotes/view">Release notes</a> |
|
||||
<a href="https://sourceforge.net/projects/openrocket/files/openrocket/1.1.9/ReleaseNotes/view">Release notes</a> |
|
||||
<a href="download.html">Other versions</a>
|
||||
</span>
|
||||
</div>
|
||||
@ -68,7 +68,7 @@
|
||||
<a href="http://sourceforge.net/donate/index.php?group_id=260357"><img src="project-support.jpg" width="88" height="32" alt="Support This Project" /> </a>
|
||||
</div>
|
||||
</div>
|
||||
<p><strong>OpenRocket</strong> is an free, fully featured model
|
||||
<p><strong>OpenRocket</strong> is a free, fully featured model
|
||||
rocket simulator that allows you to design and simulate your
|
||||
rockets before actually building and flying them.</p>
|
||||
<p>The main features include:</p>
|
||||
@ -96,6 +96,18 @@
|
||||
<div class="clear"></div>
|
||||
<div class="news">
|
||||
<h2>News</h2>
|
||||
<p><span class="date">24.11.2011:</span> Version 1.1.9 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
<p>For this version Richard Graham has implemented geodetic
|
||||
computation methods, which take into account the curvature of the
|
||||
Earth and the coriolis effect. The computation method is selected
|
||||
by the <em>Geodetic calculations</em> option in the simulation
|
||||
options. It's not <em>(yet)</em> a full spherical computation model, but
|
||||
should be accurate enough for almost all sub-orbital needs.</p>
|
||||
<p>Doug Pedrick has also enhanced the printing system with the
|
||||
ability to print fin positioning guides, transition templates and
|
||||
nose cone profiles. Other smaller enhancements and bug fixes are
|
||||
also included.</p>
|
||||
<p><span class="date">25.8.2011:</span> Version 1.1.8 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
<p>This release contains bug fixes to the optimization methods.
|
||||
|
||||
@ -1,5 +1,5 @@
|
||||
<set stableversion="1.0.0">
|
||||
<set developmentversion="1.1.8">
|
||||
<set developmentversion="1.1.9">
|
||||
<set version="${developmentversion}">
|
||||
|
||||
<def name="downloadbox">
|
||||
|
||||
@ -9,6 +9,21 @@
|
||||
|
||||
<!--- Remember to move the position of "onlyrecent" below! --->
|
||||
|
||||
<p><span class="date">24.11.2011:</span> Version 1.1.9 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
|
||||
<p>For this version Richard Graham has implemented geodetic
|
||||
computation methods, which take into account the curvature of the
|
||||
Earth and the coriolis effect. The computation method is selected
|
||||
by the <em>Geodetic calculations</em> option in the simulation
|
||||
options. It's not <em>(yet)</em> a full spherical computation model, but
|
||||
should be accurate enough for almost all sub-orbital needs.</p>
|
||||
|
||||
<p>Doug Pedrick has also enhanced the printing system with the
|
||||
ability to print fin positioning guides, transition templates and
|
||||
nose cone profiles. Other smaller enhancements and bug fixes are
|
||||
also included.</p>
|
||||
|
||||
<p><span class="date">25.8.2011:</span> Version 1.1.8 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
|
||||
@ -33,6 +48,10 @@
|
||||
instead of true physical phenomena. Always keep common sense at
|
||||
hand and take the results with a grain of salt.</p>
|
||||
|
||||
|
||||
<if not onlyrecent><!--- Older items not shown on download page: --->
|
||||
|
||||
|
||||
<p><span class="date">22.7.2011:</span> Version 1.1.6 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
|
||||
@ -46,10 +65,6 @@
|
||||
<p>The release also includes design scaling support and numerous bug
|
||||
fixes.</p>
|
||||
|
||||
|
||||
<if not onlyrecent><!--- Older items not shown on download page: --->
|
||||
|
||||
|
||||
<p><span class="date">10.6.2011:</span> Version 1.1.5 is
|
||||
<a href="download.html">released</a>!</p>
|
||||
|
||||
|
||||
Loading…
x
Reference in New Issue
Block a user