Path: Orbit/OrbitMechanics
% Time vector for a TLE Time vector for a TLE Type TLETime for a demo. -------------------------------------------------------------------------- Form: t = TLETime( tLE, startDate, endDate, n ) -------------------------------------------------------------------------- ------ Inputs ------ tLE (1,:) TLE string startDate (1,1) or (1,6) Julian date or date array endDate (1,1) or (1,6) Julian date or date array n (1,1) Number of steps (default is 100) ------- Outputs ------- t (1,n) Time vector --------------------------------------------------------------------------
Orbit: OrbitCoord/ConvertNORAD Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Time/DTSToDTA Common: Time/Date2JD
Back to the Orbit Module page