Path: Orbit/RHSOrbit
Events function for FOrbLEOP
% Its companion function is FOrbLEOP
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Form:
xDot = FOrbLEOP( t, x, d )
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Inputs
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t Time (Not used)
x (7,1) The state vector [r;v;m]
d (1,1) Data structure (Not used)
.thrust (1,1) Engine thrust (N)
.mu (1,1) Gravitational parameter
.uE (1,1) Exhaust velocity (m/s)
.cDA (1,1) Drag area product
.burnStart (1,1) Start time of burn
.burnEnd (1,1) End time of burn
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Outputs
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value (1,1) Value of stopping condition
isTerminal (1,1) 1 if terminal
direction (1,1) Direction of crossing the boundary
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