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SUPPORT SITE |
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SUPPORT SITE |
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Path: SpacecraftEstimation/DemoFuns
% Right-hand-side for a thruster based on the input pulsewidth.
t is not used. This is compatible with RK4 and RK45.
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Form:
f = RHSPressure( mFuel, t, d )
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Inputs
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x (1,1) State (fuel mass, not used)
t (1,1) Time (not used)
d (1,1) Data structure
.mDot (1,1) Mass flow
.pw (1,1) pulsewidth
.dT (1,1) Time step
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Outputs
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f (1,1) State derivative
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