Path: Missions/AlphaCentauri
% Analysis of approach orbits to Alpha Centauri binary system Alpha Centauri A-B system is in XY plane The spacecraft approaches from Earth at: 16.7 deg elevation angle to the plane -122.2 deg azimuth angle (measured from perigee of B's orbit about A) Begin approach with a hyperbolic orbit around A. You may use this as an initial condition to numerically integrate RHS to see effect of B disturbance. Use RHSAlphaCentauriMission. Since version 10. ------------------------------------------------------------------------ See also AlphaCentauriMissionAnalysis ------------------------------------------------------------------------ % -------------------------------------------------------------------------- Copyright 2011 Princeton Satellite Systems, Inc. All rights reserved. --------------------------------------------------------------------------
AC: ACData/ACTConstants Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/RVFromKepler SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/MatToCell Common: General/StringToTokens Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Mesh2 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: Transform/DMS2Rad Common: Transform/HMS2Rad Math: Linear/DupVect Math: Linear/Mag Math: Linear/Unit
Back to the Missions Module page