Path: Orbit/StraightLine
% Solve a straight-line power-limited rocket problem.
One of m0, tF, dF, or Pj fields may be empty. This field will be solved for
using the remaining problem parameters. The solution assumes the optimal
power-limited rocket trajectory which is a linear acceleration profile.
Type SLPLSolver for a demo.
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Form:
data = SLPLSolver( d, doPlot )
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Inputs
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d (.) Data structure
doPlot (1,1) If true, plot
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Outputs
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data (.) Data structure
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Reference: Leitmann, George. "Minimum Transfer Time for a Power-Limited
Rocket." Journal of Applied Mechanics 28, no. 2 (June 1,
1961): 171-78. https://doi.org/10.1115/1.3641648.
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See also: SLPLDataStructure, SLPLTrajectory
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Orbit: StraightLine/SLPLDataStructure Orbit: StraightLine/SLPLTrajectory Common: Graphics/Plot2D Common: Graphics/TimeLabl
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