Path: Orbit/RHSOrbit
Events function for FOrbLEOP % Its companion function is FOrbLEOP -------------------------------------------------------------------------- Form: xDot = FOrbLEOP( t, x, d ) -------------------------------------------------------------------------- ------ Inputs ------ 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 ------- Outputs ------- 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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