Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints

Journal of Guidance, Control, and Dynamics

Volumn 18, Issue 6, 1995, Pages 1372-1379

  Wie, Bong ^a   Lu, Jianbo ^a,b  

^a ARIZONA STATE UNIVERSITY   (United States)

^b PURDUE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ALGORITHMS; CONSTRAINT THEORY; DIFFERENTIAL EQUATIONS; DYNAMICS; EQUATIONS OF MOTION; MATRIX ALGEBRA; SENSORS; SPACECRAFT; TORQUE; VECTORS;

ANGULAR MOMENTUM VECTOR; FEEDBACK CONTROL LOGIC; QUATERNION FEEDBACK CONTROL; SPACECRAFT EIGENAXIS ROTATIONS; X RAY TIMING EXPLORER;

FEEDBACK CONTROL;

EID: 0029410445     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.21555     Document Type: Article

References (8)

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2. Bilimoria, K. D., and Wie, B., “Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft,” Journal of Guidance, Control, andDynamics, Vol 16, No. 3, 1993, pp. 446-452.
3. Wie, B., and Barba, P., “Quaternion Feedback for Spacecraft Large Angle Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, 1985, pp. 360-365.
4. Wie, B., Weiss, H., and Arapostathis, A., “Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations,” Journal of Guidance, Control, and Dynamics, Vol. 12, No. 3, 1989, pp. 375-380.
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8. Moroz, A. I., “RELION: Time-Suboptimal Variable Structure Control Law,” International Journal of Control, Vol. 52, No. 3, 1990, pp. 655-668.