Path: StraightLine/Straight2D
% Find the exhaust velocity to minimize duration using fminbnd This is the exhaust velocity that minimizes the duration for the requested mission (payload fraction, distance and specific power). Type OptimalExhaustVelocity for a demo to Jupiter. -------------------------------------------------------------------------- Form: [uEOpt,tF] = OptimalImpulseDuration( d, lambda ) -------------------------------------------------------------------------- ------ Inputs ------ d (.) Engine data structure lambda (1,1) Payload fraction ------- Outputs ------- uE (1,1) Exhaust velocity (km/s) tF (1,1) Minimum duration (s) -------------------------------------------------------------------------- See also ComputePayloadFraction --------------------------------------------------------------------------
StraightLine: Straight2D/ComputeDurationFraction StraightLine: Straight2D/Straight2DStructure Common: Database/Constant
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