Path: Orbit/StraightLine
% Compare a constant-thrust mission to optimal linear acceleration First find the constant-thrust solution for a given distance, time, and engine configuration. The 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, SLPLFindDuration, % -------------------------------------------------------------------------- Copyright (c) 2020 Princeton Satellite Systems, Inc. All rights reserved. -------------------------------------------------------------------------- Since version 2020.2 --------------------------------------------------------------------------
Orbit: StraightLine/SLPLDataStructure Orbit: StraightLine/SLPLFindMass Orbit: StraightLine/SLPLSolver Orbit: StraightLine/SLPLTrajectory Orbit: StraightLine/SimulateStraightLineTrajectory Common: Database/Constant Common: Graphics/NewFig Common: Graphics/TimeLabl DFDMissions: Straight2D/ComputeThrust DFDMissions: Straight2D/Straight2DStructure
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