Attitude maneuvers of a rigid spacecraft in a circular orbit

Proceedings of the American Control Conference

Volumn 2006, Issue , 2006, Pages 1742-1747

  Lee, Taeyoung ^a   McClamroch, N Harris ^a   Leok, Melvin ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE MANEUVERS; CIRCULAR ORBITS; EULER ANGLES; QUATERNIONS;

ATTITUDE CONTROL; BOUNDARY VALUE PROBLEMS; GRAVITATIONAL EFFECTS; OPTIMAL CONTROL SYSTEMS; ORBITS; PROBLEM SOLVING;

SPACECRAFT;

EID: 34047205704     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. P. C. Hughes, Spacecraft attitude dynamcis. John Wiley & Sons, 1986.
2. B. Wie, Space Vehicle Dynamics and Control. AIAA, 1998.
3. T. Lee, M. Leok, and N. H. McClamroch, "A Lie group variational integrator for the attitude dynamics of a rigid body with application to the 3D pendulum," in Proceedings of the IEEE Conference on Control Application, Toronto, Canada, Aug 2005, pp. 962-967.
4. _, "Lie group variational integrators for the Full Body problem," Computer Methods in Applied Mechanics and Engineering, submitted, Available: http://arxiv.org/abs/math.NA/0508365.