Large angle attitude control of spacecraft with actuator saturation

Control Engineering Practice

Volumn 11, Issue 9, 2003, Pages 989-997

  Bang, Hyochoong ^a   Tahk, Min Jea ^a   Choi, Hyung Don ^b  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^b Korea Aerospace Research Institute (KARI)   (South Korea)

Author keywords

Actuator saturation; Anti windup control; Intelligent integrator; Spacecraft large angle maneuver

Indexed keywords

ACTUATORS; CONTROL EQUIPMENT; SPACECRAFT;

INTEGRAL CONTROL SYSTEMS;

THREE TERM CONTROL SYSTEMS;

CONTROL ACTUATOR;

EID: 0141792442     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(02)00216-2     Document Type: Article

References (11)

1. Choi, H. D., Bang, H., & Kim, Z. C. (1998). Design methods for rocket attitude control systems subject to actuator saturation. Journal of Guidance, Control, and Dynamics, 21, 183-185.
2. Creamer, G., et al. (1996). Attitude determination and control of clementine during lunar mapping. Journal of Guidance, Control, and Dynamics, 19, 505-511.
3. Hanu, R., Kinnaert, M., & Henrotte, J. L. (1987). Conditioning technique, a general anti-windup and bumpless transfer method. Automatica, 23, 729-739.
4. Kothare, M. V., Campo, P. J., Morari, M., & Nett, C. N. (1994). A unified framework for the study of anti-windup designs. Automatica, 30, 1869-1883.
5. Krikelis, N. J. (1980). State feedback integral control with intelligent integrators. International Journal of Control, 32, 465-473.
6. Robinett, R. D., et al. (1997). Lyapunov optimal saturated control for nonlinear systems. Journal of Guidance, Control, and Dynamics, 20, 1083-1088.
7. Wertz, J. R. (1994). Spacecraft attitude determination and control. Netherlands: Kluwer Academic Publishers.
8. Wie, B., & Barba, P. M. (1985). Quaternion feedback for spacecraft large angle maneuvers. Journal of Guidance, Control, and Dynamics, 8, 360-365.
9. Wie, B., Heiberg, C., & Bailey, D. (2001). Rapid multi-target acquisition and pointing control of agile spacecraft. Journal of Guidance, Control, and Dynamics, 25, 96-104.
10. Wie, B., & Lu, J. (1995). Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints. Journal of Guidance, Control, and Dynamics, 18, 1372-1379.
11. Wie, B., & Weiss, H. (1989). Quaternion feedback regulator for spacecraft eigenaxis rotations. Journal of Guidance, Control, and Dynamics, 12, 375-380.