Demonstrate the playback of multiple orbits and moving sensor cones.
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See also PackageOrbitDataForPlayback and PlaybackOrbitSim, Date2JD,
OrbRate, Period, RVFromKepler
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Contents
Define epoch and simulate orbit
jD0 = Date2JD;
sma = 6800;
el = [sma, pi/4, 0, 0, 0, 0];
T = Period(sma);
n = OrbRate(sma);
time = 0:20:T*2;
[r1,v1] = RVFromKepler(el,time);
Define sensor attributes
coneFOV = pi/4;
conePitch = pi/4*abs(cos(n*time));
coneAzimuth = 0;
inputFrame = 'ECI';
Package orbit data for satellite 1
object(1) = PackageOrbitDataForPlayback( jD0, time, r1, v1,...
coneFOV, conePitch, coneAzimuth, inputFrame );
simulate second orbit
el = [sma, pi/4 + .08, 0, .08, 0, .05];
[r2,v2] = RVFromKepler(el,time);
Package orbit data for satellite 2
object(2) = PackageOrbitDataForPlayback( jD0, time, r2, v2,...
coneFOV*0.2, conePitch, coneAzimuth, inputFrame );
Load data into AnimationGUI using PlaybackOrbitSim
planet = 'EarthMR';
style = '3D';
PlaybackOrbitSim( time, object, planet, style )
