Epicyclic motion of satellites about an oblate planet

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 3, 2001, Pages 586-596

  Hashida, Y ^a   Palmer, P L ^a  

^a UNIVERSITY OF SURREY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; EQUATIONS OF MOTION; GEOMETRY; GRAVITATIONAL EFFECTS; LINEARIZATION; MATHEMATICAL MODELS; ORBITS; PERTURBATION TECHNIQUES; PLANETS; SATELLITES;

EPICYCLIC MOTION; FIRST ORDER THEORY; OBLATE PLANET;

FLIGHT DYNAMICS;

EID: 0035333997     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4750     Document Type: Article

References (13)

1. The motion of a close earth satellite
2. Solution of the problem of artificial satellite theory without drag
3. Note on the motion of a close earth satellite with a small eccentricity
4. Perturbations of near-circular orbits by the earth's gravitational potential
5. Satellite motion about an oblate planet for low and moderate eccentricities
6. On satellite orbits with very small eccentricities
7. Perturbations, untruncated in eccentricity, for an orbit in an axi-symmetric gravitational field
8. The effect of the earth's oblateness on the orbit of a near satellite
9. Effect of earth's oblateness on the anomalistic period of a satellite
10. The motion of satellite in an axi-symmetric gravitational field
11. Nodal period of an earth satellite
12. High precision integration methods for orbit modelling