The state transition matrix of relative motion for the perturbed non-circular reference orbit

Advances in the Astronautical Sciences

Volumn 108 I, Issue , 2001, Pages 913-924

  Gim, Dong Woo ^a   Alfriend, Kyle T ^a  

^a Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DIFFERENTIAL EQUATIONS; ERROR ANALYSIS; GRAVITATION; MATRIX ALGEBRA; PERTURBATION TECHNIQUES; SATELLITES;

ORBIT ECCENTRICITY;

ORBITS;

EID: 0035729987     PISSN: 10816003     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Gravitational perturbations, nonlinearity and circular orbit assumption effects on formation flying control strategies
2. Solution of the problem of artificial satellite theory without drag
3. Terminal guidance system for satellite rendezvous
4. Relative motion in highly elliptical orbits
5. Time-explicit representation of relative motion between elliptical orbits
6. Rendezvous zu einem in Elliptischer Bahn um Laufenden Ziel
7. Initial conditions and fuel-optimal control for formation flying of satellites