feat: inc/dec orbiter velocity
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@ -119,7 +119,14 @@ void ParticleMap::setParticleLocalVelocity(const std::string& id, double time, c
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newOrbit.setTrueAnomaly(keplerian[astro::trueAnomalyIndex]);
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const double newMeanAnomaly = newOrbit.getMeanAnomaly(gravitationalParameter, time);
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const double newMeanAnomalyAtEpoch = originalMeanAnomalyAtEpoch - (newMeanAnomaly - originalMeanAnomaly);
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const double meanAnomalyShift = newMeanAnomaly - originalMeanAnomaly;
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const double periapsisShift = newOrbit.getArgumentOfPeriapsis() - orbit.getArgumentOfPeriapsis();
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//const double ascendingNodeShift = newOrbit.getLongitudeOfAscendingNode() - orbit.getLongitudeOfAscendingNode();
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const double newMeanAnomalyAtEpoch = originalMeanAnomalyAtEpoch
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- meanAnomalyShift
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- periapsisShift;
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//- ascendingNodeShift;
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newOrbit.setMeanAnomalyAtEpoch(newMeanAnomalyAtEpoch);
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setRelationship(parentId, id, newOrbit);
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80
src/main.cpp
80
src/main.cpp
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@ -35,7 +35,8 @@
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struct Input
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{
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bool pauseTime;
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bool updateOrbit;
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bool prograde;
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bool retrograde;
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} input;
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@ -44,14 +45,16 @@ void keyCallback(GLFWwindow* window, int key, int scancode, int action, int mods
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if (action == GLFW_PRESS)
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{
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input.pauseTime = key == GLFW_KEY_SPACE;
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input.updateOrbit = key == GLFW_KEY_W;
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input.prograde = key == GLFW_KEY_W;
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input.retrograde = key == GLFW_KEY_S;
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}
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}
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void clearInput()
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{
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input.pauseTime = false;
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input.updateOrbit = false;
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input.prograde = false;
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input.retrograde = false;
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}
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// now should always increase linearly with real world time, this should not be modified by input
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@ -88,36 +91,43 @@ int main()
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// set parameters of moon's orbit around earth
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Orbit moonOrbit;
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double moonOrbitSemiMajorAxis = 3.84748e8;
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//double moonOrbitSemiMajorAxis = 3.84748e8;
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double moonOrbitSemiMajorAxis = 1;
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moonOrbit.setSemiMajorAxis(moonOrbitSemiMajorAxis); // metres
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moonOrbit.setEccentricity(0.055);
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moonOrbit.setInclination(glm::radians(5.15)); // radians
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moonOrbit.setArgumentOfPeriapsis(318.15); // in the case of the moon these last two values are
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moonOrbit.setLongitudeOfAscendingNode(60.0); // pretty much constantly changing so use whatever
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//moonOrbit.setEccentricity(0.055);
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//moonOrbit.setInclination(glm::radians(5.15)); // radians
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//moonOrbit.setArgumentOfPeriapsis(318.15); // in the case of the moon these last two values are
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//moonOrbit.setLongitudeOfAscendingNode(60.0); // pretty much constantly changing so use whatever
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moonOrbit.setEccentricity(0.01);
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moonOrbit.setInclination(0.0);
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moonOrbit.setArgumentOfPeriapsis(0.0);
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moonOrbit.setLongitudeOfAscendingNode(0.0);
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moonOrbit.setTrueAnomaly(0.0);
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// set parameters of satellite orbit around moon
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Orbit stationOrbit;
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stationOrbit.setSemiMajorAxis(5e7);
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stationOrbit.setEccentricity(0.6);
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stationOrbit.setInclination(glm::radians(89.0));
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stationOrbit.setArgumentOfPeriapsis(43.2);
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stationOrbit.setLongitudeOfAscendingNode(239.7);
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stationOrbit.setTrueAnomaly(0.0);
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//Orbit stationOrbit;
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//stationOrbit.setSemiMajorAxis(5e7);
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//stationOrbit.setEccentricity(0.6);
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//stationOrbit.setInclination(glm::radians(89.0));
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//stationOrbit.setArgumentOfPeriapsis(43.2);
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//stationOrbit.setLongitudeOfAscendingNode(239.7);
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//stationOrbit.setTrueAnomaly(0.0);
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ParticleMap map;
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map.setParticle({"earth", 5.9e24});
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map.setParticle({"moon", 7.3e22});
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map.setParticle({"station", 1e6});
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//map.setParticle({"earth", 5.9e24});
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//map.setParticle({"moon", 7.3e22});
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map.setParticle({"earth", 1});
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map.setParticle({"moon", .5});
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//map.setParticle({"station", 1e6});
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map.setRelationship("earth", "moon", moonOrbit);
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map.setRelationship("moon", "station", stationOrbit);
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//map.setRelationship("moon", "station", stationOrbit);
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float scale = moonOrbitSemiMajorAxis * 1.1;
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ParticleVisualizer earthVis(map, "earth", 0.1, litProgram, unlitProgram, scale);
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ParticleVisualizer moonVis(map, "moon", 0.02, litProgram, unlitProgram, scale);
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ParticleVisualizer stationVis(map, "station", 0.01, litProgram, unlitProgram, scale);
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//ParticleVisualizer stationVis(map, "station", 0.01, litProgram, unlitProgram, scale);
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OrbitVisualizer moonOrbitVis(map, "moon", unlitProgram, scale);
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OrbitVisualizer stationOrbitVis(map, "station", unlitProgram, scale);
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//OrbitVisualizer stationOrbitVis(map, "station", unlitProgram, scale);
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// register input
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glfwSetKeyCallback(window, keyCallback);
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@ -166,16 +176,18 @@ int main()
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}
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else
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{
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if (input.updateOrbit)
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//glm::dvec3 v = map.getParticleLocalVelocity("station", time);
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glm::dvec3 v = map.getParticleLocalVelocity("moon", time);
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if (input.prograde)
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{
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const glm::dvec3 p = map.getParticleLocalPosition("station", time);
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const glm::dvec3 v = map.getParticleLocalVelocity("station", time);
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const glm::dvec3 newVelocity = v * 0.99;
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map.setParticleLocalVelocity("station", time, newVelocity);
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v *= 1.01;
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}
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else if (input.retrograde)
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{
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v *= 0.99;
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}
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//map.setParticleLocalVelocity("station", time, v);
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map.setParticleLocalVelocity("moon", time, v);
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}
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// rendering
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@ -186,17 +198,17 @@ int main()
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const Particle& earth = map.getParticle("earth");
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const Particle& moon = map.getParticle("moon");
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moonOrbit = map.getOrbit("moon");
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stationOrbit = map.getOrbit("station");
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//stationOrbit = map.getOrbit("station");
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moonOrbit.update(time, earth.getGravitationalParameter());
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stationOrbit.update(time, moon.getGravitationalParameter());
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//stationOrbit.update(time, moon.getGravitationalParameter());
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map.setRelationship("earth", "moon", moonOrbit);
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map.setRelationship("moon", "station", stationOrbit);
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//map.setRelationship("moon", "station", stationOrbit);
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earthVis.render(time);
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moonVis.render(time);
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stationVis.render(time);
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//stationVis.render(time);
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moonOrbitVis.render(time);
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stationOrbitVis.render(time);
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//stationOrbitVis.render(time);
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glfwSwapBuffers(window);
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}
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