|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
Path: Orbit/OrbitMechanics
% Batch form of RV2El. Enforces continuous true anomaly for an osculating orbit. Handles special cases like equatorial and circular orbits. The numerical tolerance should be consistent with that used to generate the
Common: Graphics/Plot2D Common: Time/Date2JD Math: Linear/Cross Math: Linear/Dot Math: Linear/Mag Orbit: OrbitMechanics/J2Prop OrbitMiniToolbox: Support/El2RV SC: BasicOrbit/E2M SC: BasicOrbit/Nu2E SC: BasicOrbit/Period
Back to the Orbit Module page