Lagrange perturbation equations for noninertial reference systems
Abstract
In order to calculate satellite orbital element perturbations in a noninertial reference system, the usual form of the Lagrangian perturbation equations for inertial reference systems are expressed in the noninertial systems and the element perturbations are calculated directly in the corotating systems on the resulting relationships.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- 1974
- Bibcode:
- 1974STIN...7524793R
- Keywords:
-
- Artificial Satellites;
- Euler-Lagrange Equation;
- Inertial Reference Systems;
- Orbit Perturbation;
- Satellite Orbits;
- Geodesy;
- Orbital Elements;
- Orbital Mechanics;
- Astrodynamics