New state transition matrix for relative motion on an arbitrary elliptical orbit

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 1, 2002, Pages 60-66

  Yamanaka, Koji ^a   Ankersen, Finn ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b EUROPEAN SPACE AGENCY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; LINEAR EQUATIONS; LINEARIZATION; MATRIX ALGEBRA; ORBITS;

ARBITRARY ELLIPTICAL ORBITS;

AEROSPACE ENGINEERING;

EID: 0036154546     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4875     Document Type: Article

References (4)

1. State transition matrices for terminal rendezvous studies: Brief survey and new example
2. Strategies and schemes for rendezvous on geostationary transfer orbit
3. Time-explicit representation of relative motion between elliptical orbits
4. New form for the optimal rendezvous equations near Keplerian orbit