Path: StraightLine/SLPowerLimited
% Compare a constant-thrust mission to optimal linear acceleration First find the constant-thrust solution for a given distance, time, and engine configuration. Then compute the equivalent optimal mission in two cases: 1. the fuel is 100% consumed and the trip is shorter; 2. the trip is the same duration and the saved fuel mass can be extra payload. See also: Straight2DStructure, ComputeThrust, SLPLSolver, SLPLDataStructure % -------------------------------------------------------------------------- Copyright (c) 2020 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since version 2020.2 --------------------------------------------------------------------------
StraightLine: ConstantThrust/SimulateStraightLineTrajectory StraightLine: SLPowerLimited/SLPLDataStructure StraightLine: SLPowerLimited/SLPLFindMass StraightLine: SLPowerLimited/SLPLSolver StraightLine: SLPowerLimited/SLPLTrajectory StraightLine: Straight2D/ComputeThrust StraightLine: Straight2D/Straight2DStructure Common: Database/Constant Common: Graphics/NewFig Common: Graphics/TimeLabl
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