Path: LunarMissions/LunarRHS
% Simple thruster force model for orbit simulations
Models the force for a thruster using a direction vector and a scalar
magnitude.
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Form:
d = ForceSimple; % default data structure
f = ForceSimple( d )
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Inputs
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d (.) Data structure
.uThrustECI (3,1) Thrust unit vector in the ECI frame
.thrustMag (1,1) Thrust magnitude (N)
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Outputs
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f (3,1) ECI force vector (N)
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