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 --------------------------------------------------------------------------