The low-eccentricity earth satellite orbit at the critical inclination |
| |
| Authors: | R H Lyddane Charles J Cohen |
| |
| Institution: | (1) Ebeling Associates, 1 Glen Ave., 12302 Scotia, N.Y., USA;(2) Naval Surface Weapons Center, 22448 Dahlgren, Va., USA |
| |
| Abstract: | A solution to the orbital motion of an Earth satellite at the critical inclination and with near-zero eccentricity is developed by the von Zeipel method to the first order in the eccentricity, and to the first order in the higher gravitational harmonics, using elements which do not degenerate at zero eccentricity. |
| |
| Keywords: | |
| 本文献已被 SpringerLink 等数据库收录！ |
|
