EarthOrbitDragDemo:

Path: Orbit/OrbitSim

% Simple demo to compute drag over one orbit 
  Assumes point mass s/c, two body propagation. The only perturbing 
  acceleration considered is due to drag. Mass is assumed to be constant, 
  fixed cross-sectional area and drag coefficient. Demo produces plots of
  spacecraft position and velocity (in ECI frame) and drag force (N) (in 
  ECI frame). DV due to drag perturbation is displayed.

  Since version 11
 -------------------------------------------------------------------------
  See also:    Constant, Date2JD, Period, RVFromKepler,
  SolarFluxPrediction, AtmJ70, EarthRte, Skew, ECIToEF, FOrbCart, Mag,
  TimeLabl,Plot2D, 
 -------------------------------------------------------------------------
%
 -------------------------------------------------------------------------
   Copyright (c) 2013 Princeton Satellite Systems, Inc.
   All rights reserved.
 -------------------------------------------------------------------------

Children:

AC: ACData/ACTConstants
AerospaceUtils: AtmosphericCalculations/AtmJ70
AerospaceUtils: AtmosphericCalculations/BaromExp
AerospaceUtils: AtmosphericCalculations/DiffusionExp
AerospaceUtils: Coord/ECIToEF
SC: BasicOrbit/Period
SC: BasicOrbit/RVFromKepler
SC: Environs/SolarFluxPrediction
SC: Ephem/EarthRte
SC: Ephem/MSidDay
SC: Ephem/SunV1
SC: SCData/sCTConstants
SC: SCMat/SolarFluxPredictions
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: Database/Constant
Common: FileUtils/FindDirectory
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/Plot3D
Common: Graphics/PltStyle
Common: Graphics/TimeLabl
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: Time/DTAToDTS
Common: Time/DTSToDTA
Common: Time/Date2DN
Common: Time/Date2JD
Common: Time/JD2DN
Common: Time/JD2Date
Common: Time/JD2T
Common: Time/T2JD
Math: Integration/RK4
Math: Linear/Mag
Math: Linear/Skew
Math: Linear/Unit
Math: MathUtils/R2P5
Math: Trigonometry/ACosD
Math: Trigonometry/CosD
Math: Trigonometry/SinD

Back to the Orbit Module page