Path: Orbit/OrbitMechanics
% Computes the asymptote angle for a hyperbola. If e is < 1 it substitutes 1. Since version 1. -------------------------------------------------------------------------- Form: psi = NuInf( e ) -------------------------------------------------------------------------- ------ Inputs ------ e Eccentricity ------- Outputs ------- psi Asymptote angle -------------------------------------------------------------------------- References: Wiesel, W. E., Spaceflight Dynamics, McGraw-Hill, 1988, pp. 54. --------------------------------------------------------------------------
Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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