Retrofit Reconfigurable Flight Control in the presence of control effector damage

Proceedings of the American Control Conference

Volumn 4, Issue , 2005, Pages 2652-2657

  Bošković, Jovan D ^a   Bergstrom, Sarah E ^a   Mehra, Raman K ^a  

^a SCIENTIFIC SYSTEMS COMPANY INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMAGE ADAPTIVE CONTROL SYSTEM; FLIGHT CRITICAL ACTUATORS; INTEGRATED RETROFIT RECONFIGURABLE FLIGHT CONTROL; VARIABLE STRUCTURAL CONTROL (VSC);

ACTUATORS; ALGORITHMS; CONTROL NONLINEARITIES; FAILURE (MECHANICAL); FLIGHT DYNAMICS; STRUCTURAL ANALYSIS;

ADAPTIVE CONTROL SYSTEMS;

EID: 23944454471     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. F. Ahmed-Zaid, P. Ioannou, K. Gousman and R. Rooney, "Accommodation of Failures in the F-16 Aircraft using Adaptive Control", IEEE Control Systems Magazine, 11(1), 73-78, January 1991.
2. M. Bodson and J. Groszkiewicz, "Multivariable Adaptive Algorithms for Reconfigurable Flight Control", IEEE Transactions on Control Systems Technology, 5(2), 217-229, March 1997.
3. Boeing Phantom Works, "Reconfigurable Systems for Tailless Fighter Aircraft - RESTORE", Contract No. F33615-96-C-3612, System Design Report A007, St. Louis, Missouri, May 1998.
4. J. D. Boskovic et al. "Adaptive Accommodation of Failures in Second-Order Flight Control Actuators with Measurable Rates", to be presented at the 2005 ACC, Portland. OR, June 8-10, 2005.
5. J. D. Boskovic et al. "Performance Evaluation of an Integrated Retrofit Failure Detection, Identification and Reconfiguration (FDIR) System using High-Fidelity and Piloted Simulations", in Proc. 2004 SAE World Aviation Congress, Reno, NV, Nov. 2004.
6. J. D. Bošković, L. Chen and R. K. Mehra, "Adaptive Control Design for a Class of Non-Affine Models Arising in Flight Control", AIAA J. Guidance. Control & Dynamics, 27(2), 209-217, March 2004.
7. J. D. Bošković and R. K. Mehra, "Robust Fault-Tolerant Control Design for Aircraft Under State-Dependent Disturbances", Proc. 2003 AIAA GNC, Austin, TX, August 11-14, 2003.
8. J. D. Bošković and R. K. Mehra, "A Decentralized Scheme for Autonomous Compensation of Multiple Simultaneous Flight-Critical Failures", Proc. 2002 AIAA GNC, Monterey, CA, August 2002.
9. J. D. Bošković and R. K. Mehra, "Adaptive Retrofit Reconfigurable Flight Control", Proc. 41st CDC, Las Vegas, NV, Dec. 2002.
10. J. D. Bošković and R. K. Mehra, "A Multiple Model Adaptive Right Control Scheme for Accommodation of Actuator Failures", AIAA J. Guidance, Control & Dynamics, 25(4), 712-724, July 2002.
11. J. D. Bošković and R. K. Mehra, "An Adaptive Scheme for Compensation of Loss of Effectiveness of Flight Control Effectors", Proc. 40th IEEE CDC, Orlando, FL, Dec. 2001.
12. J. D. Bošković and R. K. Mehra, "Intelligent Adaptive Control of a Tailless Advanced Fighter Aircraft under Wing Damage", AIAA J. of Guidance. Control & Dynamics, 23(5), 876-884, Sept. 2000.
13. J. Brinker and K. Wise, "Reconfigurable Flight Control of a Tailless Advanced Fighter Aircraft", Proc. AIAA GNC, Boston, MA, 1998.
14. A. Calise, S. Lee and M. Sharma, "Direct Adaptive Reconfigurable Control of a Tailless Fighter Aircraft", Proc. AIAA GNC, Boston, MA, Aug. 1998.
15. P. Chandler, M. Pachter and M. Mears, "System Identification for Adaptive and Reconfigurable Control", J. Guidance, Control & Dynamics, 18(3), 516-524, May 1995.
16. L. Hsu and R. Costa, "Variable Structure Model Reference Adaptive Control using only I/O Measurements", Int. Journal of Control, 49 (2), pp. 399-416, 1989.
17. K. S. Narendra and A. M. Annaswamy, Stable Adaptive Systems, Prentice Hall Inc., Englewood Cliffs, New Jersey, 1988.
18. M. D. Tandale and J. Valasek, "Structured Adaptive Model Inversion Control to Simultaneously Handle Actuator Failure and Actuator Saturation", Proc. AIAA GNC, Austin, TX. Aug. 2003.