Genetic programming of spacecraft attitude maneuvers under reaction wheel control

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-12

  Howley, Brian ^a  

^a LOCKHEED MARTIN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GENETIC ALGORITHMS; SPACECRAFT; WHEELS;

GENERAL SOLUTIONS; MINIMUM TIME CONTROL; OPTIMAL SOLUTIONS; REACTION WHEELS; RIGID SPACECRAFT; SPACECRAFT ATTITUDE MANEUVERS; TRAJECTORY PLANNING;

GENETIC PROGRAMMING;

EID: 84959152087     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Banerjee, Arun K. 1991. Optimal Feedback Gains for Three-Dimensional Large Angle Slewing of Spacecraft. Journal of Guidance, Control, and Dynamics. Volume 14. Pages 1313-1315.
2. Bilimoria, Karl D. and Wie, Bong. 1993. Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft. Journal of Guidance, Control, and Dynamics. Volume 16. Pages 446-452.
3. Beyers, R. M. and Vadali, S. R. 1993. Quasi-Closed-Form Solution to the Time-Optimal Rigid Spacecraft Reorientation Problem. Journal of Guidance, Control, and Dynamics. Volume 16. Pages 453-461.
4. Bryson, Arthur E. and Ho, Yu-Chi. 1975. Applied Optimal Control. Washington DC: Hemisphere Publishing.
5. Koza, John R. 1992. Genetic Programming: On the Programming of Computers by Means of Natural Selection. Cambridge, MA: The MIT Press.
6. Howley, Brian. 1996. Genetic Programming of Near-Minimum-Time Spacecraft Attitude Maneuvers. Genetic Programming 1996: Proceedings of the First Annual Conference, (Stanford University) July 28-31, 1996. Pages 98-109.
7. Scrivener, Sandra L. and Thompson, Roger C. 1994. Survey of Time-Optimal Attitude Maneuvers. Journal of Guidance, Control, and Dynamics. Volume 17. Pages 225-233
8. Wertz, James R. (editor). 1978. Spacecraft Attitude Determination and Control. Dordrecht, The Netherlands: Kluwer Academic Publishers.
9. Wie, Bong, and Barba, Peter M. 1985. Quaternion Feedback for Spacecraft Large Angle Maneuvers. Journal of Guidance, Control, and Dynamics. Volume 8. Pages 360-365.