ViewHills:
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Given the reference orbital elements, a time span, and the spacecrafts'
orbital elements, animate the relative motion.
Since version 7.
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Form:
ViewHills( el0, el, timeSpan, method )
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Inputs
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el0 (1,6) reference orbital elements [a i W w e M]
el (k,6) orbital elements of each spacecraft
timeSpan (1) length of time to propagate
method (:) method of propagation ('relative','keplerian','hi-fi')
( 1 2 3 )
- for method 1, first 3 inputs are: -
w0 (1,1) orbital rate [rad/s]
xH (6,k) initial Hills state [km; km/s]
timeSpan (1)
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Outputs
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sc data structure of relative positions over time
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Children:
Common: Time/Date2JD
FormationFlying: Dynamics/HillsEqns
FormationFlying: Transformation/ECI2Hills
Orbit: OrbitMechanics/J2Prop
Orbit: OrbitMechanics/RVOrbGen
OrbitMiniToolbox: Support/El2RV
Plotting: GUI/AnimationGUI
