Path: StraightLine/Flyby
% Find exhaust velocity to maximise payload fraction (fminsearch) Find the best exhaust velocity given the distance and target time -------------------------------------------------------------------------- Form: [uEOpt,lambda] = FlybyOptimalImpulse( d ) -------------------------------------------------------------------------- ------ Inputs ------ d (.) Engine data structure See Straight2DStructure ------- Outputs ------- P (1,1) Power (MW) m0 (1,1) Initial mass (kg) -------------------------------------------------------------------------- See also ZeroPayloadFlyby, SolveLambdaFlyby --------------------------------------------------------------------------
StraightLine: ConstantThrust/Straight2DStructure StraightLine: Flyby/SolveLambdaFlyby StraightLine: Flyby/ZeroPayloadFlyby Common: Database/Constant
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