Stability analysis of planetary satellite orbiters: Application to the Europa orbiter

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 4, 2001, Pages 778-787

  Scheeres, D J ^a   Guman, M D ^b   Villac, B F ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

^b CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; GRAVITATIONAL EFFECTS; MATHEMATICAL MODELS; ORBITS; SOLAR SYSTEM; SPACE FLIGHT; SYSTEM STABILITY;

ORBIT DYNAMICS; PLANETARY SATELLITE ORBITERS; STABILITY ANALYSIS;

SATELLITES;

EID: 0035394714     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4778     Document Type: Article

References (13)

1. The restricted hill four-body problem with applications to the earth-moon-sun system
2. Numerical exploration of the restricted problem. V
3. Dynamics of binary asteroids. I
4. Dynamics of distant moons of asteroids
5. Europa orbiter mission trajectory design
6. On symmetric central configurations with application to satellite motion about rings