Direct adaptive control treatment to loss of attitude control actuators

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 2, Issue , 2007, Pages 1319-1332

  Lam, Quang M ^a,c   Barkana, Itzhak ^b,c  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b Kulicke and Soffa Industries Inc   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; FAILURE ANALYSIS; FLIGHT CONTROL SYSTEMS; GEOSTATIONARY SATELLITES;

ADAPTIVE CONTROLLERS; ATTITUDE CONTROL SUBSYSTEMS (ACS); SIMPLE ADAPTIVE CONTROL (SAC);

ADAPTIVE CONTROL SYSTEMS;

EID: 37249068502     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-6435     Document Type: Conference Paper

References (7)

1. Lam, Q.M., Sanneman, P., Stamatakos, N. Vogt, B. and Kim, J. "A Mixed-Mode Attitude Control System Strategy for Actuator Failure Accommodation," AIAA Paper 2001-4156, GN&C Conference, 2001
2. Lam, Q., Barkana, L, "Direct Adaptive Control Treatment to Flight Control Input Saturation," AIAA-056179, From: AIAA Guidance, Navigation, and Control Conference, San Francisco, CA, August 16-19, 2005.
3. Krishnan, H., Mc Clamroch, N.H., Reyhanoglu, M., "Attitude stabilization of a rigid spacecraft using two momentum wheel actuators", Journal of Guidance, Control and Dynamics, 18(2), 1995, pp. 256-263.
4. Kim, S., and Kim, Y., "Spin Axis Stabilization of a Rigid Spacecraft Using Two Reaction Wheels," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 5, 2001, pp. 1046-1049.
5. Boyer, F. and Alamir, M., "Further Results on the Controllability of a Two-Wheeled Satellite", Journal of Guidance, Control and Dynamics, 30(2), 2007, pp. 611-619.
6. http://fuse.pha.jhu.edu/educ/RW_FAQ.html
7. J. W. Kruk, B. F. Class, D. Rovner, J. Westphal, T. B. Ake, H. W. Moos, B. Roberts, and L. Fisher, "FUSE In-orbit Attitude Control with Two Reaction Wheels and No Gyroscopes," 2002, SPIE, vol. 4854, paper 72