Large angle slew maneuvers with autonomous sun vector avoidance

Journal of Guidance, Control, and Dynamics

Volumn 17, Issue 4, 1994, Pages 875-877

  McLnnes, Colin R ^a  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL METHODS; CONSTRAINT THEORY; EQUATIONS OF MOTION; FLEXIBLE STRUCTURES; LYAPUNOV METHODS; MECHANICAL VARIABLES CONTROL; NAVIGATION; SATELLITES; SPACE FLIGHT; SYSTEM STABILITY; TOPOLOGY; VECTORS;

AUTONOMOUS SUN VECTOR AVOIDANCE; LARGE ANGLE SLEW MANEUVERS;

MANEUVERABILITY;

EID: 0028467924     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.21283     Document Type: Article

References (4)

1. Ximenez de Ferran, S., “The ISO Spacecraft,” ESA Bulletin, No. 67, 1991, pp. 17-24.
2. Oh, H. S., and Vadali S. R., “Feedback Control and Steering Laws for Spacecraft Using Single Gimbal Control Moment Gyros,” Journal of Astronautical Sciences, Vol. 39, No. 2, 1991, pp. 183-203.
3. Wie, B., and Barba, P. M., “Quaternion Feedback for Spacecraft Large Angle Maneuvers,” Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, 1985, pp. 360-365.
4. McInnes, C. R., “Path Constrained Manoeuvering Using Artificial Potential Functions,” Univ. of Glasgow, Dept, of Aerospace Engineering Rept. 9248, Glasgow, Scotland, UK, Dec. 1992.