Control allocation based reconfigurable flight control system design

ICIC Express Letters

Volumn 3, Issue 3, 2009, Pages 689-694

  Wang, Huidong ^a   Yu, Zirui ^a   Yi, Jianqiang ^a   Fan, Guoliang ^a  

^a INSTITUTE OF AUTOMATION   (China)

Author keywords

Dynamic control allocation; Nonlinear dynamicinversion; Reconfigurable flight control

Indexed keywords

ACTUATOR FAULT; CONTROL ALLOCATION; CONTROL LAWS; DYNAMIC CONTROL ALLOCATIONS; FLIGHT CONTROL LAW; NONLINEAR DYNAMIC INVERSION; RATE CONSTRAINTS; RE-CONFIGURABLE; RECONFIGURABLE CONTROL; RECONFIGURABLE FLIGHT CONTROL; SIMULATION RESULT; SIX DEGREE-OF-FREEDOM; TIME SCALE SEPARATION;

ACTUATORS; AIRCRAFT CONTROL; CONTROL THEORY; PNEUMATIC CONTROL EQUIPMENT;

FLIGHT CONTROL SYSTEMS;

EID: 77953889807     PISSN: 1881803X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (10)

1. M. Bodson, Evaluation of optimization methods for control allocation,Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4, pp. 703-711, 2002.
2. J. J. Burken, P. Lu, Z. L. Wu, et al., Two reconfigurable flight-controldesign methods: Robust servomechanism and control allocation, Journal ofGuidance, Control, and Dynamics, Vol. 24, No. 3, pp. 482-493, 2001.
3. G. Tao, S. Chen and S. M. Joshi, An adaptive control scheme for systemswith unknown actuator failures, Automatica Vol. 38, No. 6, pp. 1027-1034, 2002.
4. D. H. Shin and Y. Kim, Nonlinear discrete-time reconfigurable flightcontrol law using neural networks, IEEE Trans. on Control Systems Technology,Vol. 14, No. 3, pp. 408-422, 2006.
5. R. P. Costa Q. P. Chu and J. A. Mulder, Reentry flight controller designusing nonlinear dynamic inversion, Journal of Guidance, Control, and Dynamics,Vol. 40, no. 1, pp. 64-71, 2003.
6. J. Kawaguchi, Y. Miyazawa and T. Ninomiya Flight control law design withhierarchy-structured dynamic inversion approach, AIAA Guidance, Navigation, andControl Conference, Hawaii, 2008.
7. D. M. Acosta and S. S. Joshi, Actaptive nonlinear dynamic inversioncontrol of an autonomous airship for the exploration of Titan, AIAA Guidance,Navigation, and Control Conference, Hilton Head, CA, 2007.
8. K. C. Yao, Reliable robust output feedback stabilizing computer controlof decentralized stochastic singularly-perturbed systems, ICIC Express Letters,Vol. 1, no. 1, pp. 1-7, 2007.
9. B. M. Min, E. T. Kim and M. J. Tahk, Application of control allocationmethods to SAT-II UAV, AIAA Guidance, Navigation, and Control Conference, SanFrancisco, California 2005.
10. O. Härkegård, Dynamic control allocation using constrainedquadratic programming, Journal of Guidance, Control, and Dynamics, Vol. 27, No.6, pp. 1028-1034, 2004.