A mixed-mode attitude control system strategy for actuator failure accommodation

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Lam, Quang ^a   Sanneman, Paul ^a   Stamatakos, Nick ^a   Vogt, Bob ^a   Kim, Jinho ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894438783     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. M. Psiaki, Magnetic Torquer Attitude Control Via Asymtotic Periodic Linear Quadratic Regulation, Proceedings of the AIAA GN&C 2000
2. Kailath, T., Linear Systems. Prentice Hall, Englewood Cliffs, N. J., 1980
3. H. Kwakernaak & R. Sivan, Linear Optimal Control Systems, Wiley-Interscience, 1972
4. Stickler, Craig, Alfriend, K., Elementary Magnetic Attitude Control System, Journal of Spacecraft and Rockets, Vol. 13, No. 5, 1974.
5. Martel, F, Pal, P.K., and Psiaki, M.L., Active Magnetic Control System for Gravity Gradient Stabilized Spacecraft, Proceedings of the 2nd Annual AIAA/USU Conf on Small Satellites, Sept. 1988, Logan, Utah.
6. Musser, K., Ebert, W., Autonomous Spacecraft Attitude Control Using Magnetic Torquing Only, Proceedings of the Flight Mechanics/Estimation Theory Symposium, NASA Goddard Space Flight Center, Greenbelt, MD, May 1989, pp. 23-28.
7. Wisniewski, R., "Linear Time-Vary ing Approach to Satellite Attitude Control Using Only Electromagnetic Actuation," Journal of Guidance, Navigation, and Control, Vol. 23, No. 4, July- August 2000, pp. 640-647.