Hello,
Recently, I’m trying to add Box-Wing model for a square satellite in AbstractOrbitDetermination(orekit-tutorials). And I have a question.
The material of satellite body and solar panel is different, which means they should have different drag coefficients and solar absorption/reflection coefficients. But in BoxAndSolarArraySpacecraft there is only one coefficients for drag or solar absorption/reflection. Does this mean that when I want to add an atmospheric drag model to this satellite, I need to build an atmospheric drag model for the satellite itself and solar panels respectively? Such as:
// Set satellite body's drag
final ParameterDriver[] satelliteBodyDrag = setDrag(propagatorBuilder, atmosphere,
new IsotropicDrag(area, cd));
// Set solar panel's drag
final BoxAndSolarArraySpacecraft solarPanel = new BoxAndSolarArraySpacecraft(spaceCraft.getBoxSize()[0], spaceCraft.getBoxSize()[1],
spaceCraft.getBoxSize()[2],
CelestialBodyFactory.getSun(), spaceCraft.getSolarArrayArea(), solarArrayAxis, cd, ca, cr);
final ParameterDriver[] solarPanelDrag = setDrag(propagatorBuilder, atmosphere, boxCraft);
Or I just need to use BoxAndSolarArraySpacecraft to model the atmospheric drag? Like this:
// Set satellite body && solar panel's drag
final BoxAndSolarArraySpacecraft solarPanel = new BoxAndSolarArraySpacecraft(spaceCraft.getBoxSize()[0], spaceCraft.getBoxSize()[1],
spaceCraft.getBoxSize()[2],
CelestialBodyFactory.getSun(), spaceCraft.getSolarArrayArea(),
solarArrayAxis, cd, ca, cr);
final ParameterDriver[] solarPanelDrag = setDrag(propagatorBuilder, atmosphere, boxCraft);
Thank you very much!!