Path: Orbit/StraightLine
% Print a summary of an SLPL problem
tau is the time in the second half of the trajectory, between the turnaround
and tF. It is zero for a flyby, tF/2 for a rendezvous, and a value inbetween
gives a non-zero final velocity.
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Form:
[s,dOut] = SLPLReport( Pj, m0, tF, A, tau )
[s,dOut] = SLPLReport( Pj, m0, tF, A, tau, sigma, f, doPlot )
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Inputs
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Pj (1,1) Jet power (eta*P, eta*sigma*mE) (W)
m0 (1,1) Initial (wet) mass (kg)
tF (1,1) Final time (s)
A (1,1) Acceleration scale parameter, (m/s^3)
tau (1,1) Time between turnaround and tF (s)
sigma (1,1) Specific power (W/kg)
f (1,1) Tank mass fraction, mTank = f*mF
doPlot (1,1) Always display output
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Outputs
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s {} Latex report
dOut (.) Output data structure
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AC: ACData/ACTConstants Orbit: StraightLine/SLPLDeltaV Orbit: StraightLine/SLPLTrajectory SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeleteCell Common: General/DisplayLatexTable Common: General/MatToCell Common: General/Watermark Common: Graphics/DistanceLabel Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl
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