Calculation of the special functions in the satellite motion theoriesin nonsingular elements.
Abstract
The formulas and the subroutines for computing the functions appearing in the Lagrange equations of artificial satellite motion for the eccentricity 0 ≤ e < 1 and the inclination i ≠ π are presented.
- Publication:
-
Algoritm. Nebesnoj Mekhanik
- Pub Date:
- 1988
- Bibcode:
- 1988AlNM...55...18T
- Keywords:
-
- Artificial Satellites:Computing;
- Artificial Satellites:Motions