FFEccDeltaElem2Hills:
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Convert element differences to Hills frame coordinates in an eccentric orbit.
Since version 7.
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Usage:
xH = FFEccDeltaElem2Hills(el0,dEl,type);
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Inputs
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el0 (1,6) Initial reference orbital elements
dEl (1,6) Initial orbital element differences
type (1) Element set type
- 1 [a,theta,i,q1,q2,W] (Alfriend format)
- 2 [a,i,W,w,e,M] (standard format)
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Outputs
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xH (6,1) Hills frame state [x;y;z;dx/dt;dy/dt;dz/dt]
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Children:
Common: Database/Constant
FormationFlying: Transformation/ECI2Hills
Orbit: OrbitCoord/Alfriend2El
OrbitMiniToolbox: Support/El2RV
SC: BasicOrbit/OrbRate
