On-off attitude control of flexible satellites

Journal of Guidance, Control, and Dynamics

Volumn 9, Issue 4, 1986, Pages 507-510

  Skaar, S B ^a   Tang, L ^a   Yalda Mooshabad, I ^a  

^a IOWA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEMS, BANG BANG;

FLEXIBLE SATELLITES; IMPULSE RESPONSE; ON-OFF ATTITUDE CONTROL;

SATELLITES;

EID: 0022757383     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.20140     Document Type: Article

References (4)

1. Wie, B. and Barba, P. M., “Quaternion Feedback for Spacecraft Large Angle Maneuvers,” AIAA Paper 84-1032, May 1984.
2. Break well, J., “Optimal Feedback Slewing of Flexible Spacecraft,”Journal of Guidance and Control, Vol. 4, 1981, pp. 472-479.
3. Turner, J. D. and Chun, H. “Optimal Distributed Control of a Flexible Spacecraft During a Large-Angle Maneuver,”Jounal of Guidance, Control, and Dynamics, Vol. 7, 1984, pp. 257-264.
4. Skaar, S. B., “Closed Form Optimal Control Solutions for Continuous Linear Elastic Systems,”Journal of the Astronautical Sciences, Vol. 32, No. 4, Oct.-Dec., 1984.