Path: FormationFlying/Analysis
% Test the FFEccLinOrb function.
An initial reference state in the ECI frame is provided, along with an initial
relative state in Hill's frame.
First, the relative state is propagated one time-step dT using FFEccLinOrb,
with the given acceleration in Hill's frame applied.
Next, we integrate the reference and secondary states in the ECI frame,
applying the given accleration (now transformed to ECI). We then
transform the two resulting ECI states back to the Hill's frame and
compare.
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Form:
[xH_int,xH_lin] = TestFFEccLinOrb( x0, xH0, dT, aH );
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Inputs
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x0 (6,1) ECI position and velocity of reference
[km; km/s]
xH0 (6,1) Hill's-frame position and velocity of relative sat
[km; km/s]
dT (1) Time-step to integrate over [sec]
aH (3,1) Acceleration to be applied (in Hill's frame)
[km/s/s]
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Outputs
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xH_int (6,1) Hill's-frame state from integrating inertial states
xH_lin (6,1) Hill's-frame state from propagating linear system
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FormationFlying: Coord/GetHillsMats FormationFlying: EccDynamics/FFEccDH FormationFlying: EccDynamics/FFEccDiscreteHills FormationFlying: EccDynamics/FFEccGoals FormationFlying: EccDynamics/FFEccLinOrb FormationFlying: EccDynamics/FFEccProp FormationFlying: EccDynamics/FFEccRMat FormationFlying: EccDynamics/FFEccYExt EccDynamics: Derivatives/FFEccDDY EccDynamics: Derivatives/FFEccDY FormationFlying: Transformation/ECI2Hills FormationFlying: Transformation/Hills2ECI FormationFlying: Utility/NuDot FormationFlying: Visual/FFEccAnalyzeShape SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/OrbRate SC: BasicOrbit/RV2El Common: CommonData/SwooshWatermark Common: Control/C2DZOH Common: General/CellToMat Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Integration/RK4TI Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Solvers/NewtRaph Math: Trigonometry/UnwrapPhase Math: Trigonometry/WrapPhase
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