Epicyclic motion of satellites under rotating potential

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 3, 2002, Pages 571-581

  Hashida, Yoshikazu ^a   Palmer, Philip L ^a  

^a UNIVERSITY OF SURREY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; HARMONIC ANALYSIS; INTEGRATION; MATHEMATICAL MODELS; NUMERICAL METHODS; ORBITAL TRANSFER; PERTURBATION TECHNIQUES; SATELLITES;

NUMERICALLY INTEGRATED ORBITS; PERTURBED ORBITS; POSITIONAL ERROR; SATELLITES EPICYCLIC MOTION; SECOND ZONAL HARMONIC; TESSERAL HARMONIC POTENTIAL;

MOTION CONTROL;

EID: 0036563971     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4919     Document Type: Article

References (14)

1. The motion of a close earth satellite
2. Solution of the problem of artificial satellite theory without drag
3. The motion of satellite in an axi-symmetric gravitational field
4. Perturbations of near-circular orbits by the earth's gravitational potential
5. Epicyclic motion of satellites about an oblate planet
6. On the motion of a satellite in an asymmetrical gravitational field
7. Perturbations of satellite orbits by Tesseral harmonics in the earth's gravitational potential
8. Effect of ellipticity of the equator on 24-hour nearly circular satellite orbits
9. Tesseral resonance effects on satellite orbits
10. Analysis of the TOPEX/poseidon operational orbit: Observed variations and why
11. High precision integration methods for orbit modelling