An integrated approach to damage accommodation in flight control

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  Bošković, Jovan D ^a,c   Knoebel, Nathan ^a,c   Mehra, Raman K ^a,c   Gregory, Irene ^b,d  

^a SCIENTIFIC SYSTEMS COMPANY INC   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c MS 308 ^*

^d Dynamic Systems and Control Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT CONTROL; FLIGHT ENVELOPES; INTEGRATED CONTROL; ROBUST CONTROL; ROBUSTNESS (CONTROL SYSTEMS); STRUCTURAL DYNAMICS; UNCERTAINTY ANALYSIS;

CONTROL EFFECTOR DAMAGE; INTEGRATED APPROACH; NONLINEAR CROSS-COUPLING TERMS; PLACEMENT STRATEGY; STABILITY AND ROBUSTNESS; STRUCTURAL DYNAMICS MODELS; UNCERTAIN PARAMETERS; VARIABLE STRUCTURES;

CONTROLLERS;

EID: 77953737181     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6504     Document Type: Conference Paper

References (20)

1. J. D. Bošković, N. Knoebel and R. K. Mehra "An Initial Study of a Combined Robust and Adaptive Control Approach to Guaranteed Performance Flight Control", to be presented at the 2008 American Control Conference, Seattle, WA, June 11-13, 2008.
2. J. D. Bošković and R. K. Mehra, "Robust Integrated Flight Control Design Under Failures, Damage and State-Dependent Disturbances", AIAA Journal of Guidance, Control & Dynamics, Vol. 28, No. 5, pp. 902-917, September-October 2005.
3. J. D. Bošković, S. E. Bergstrom, R. K. Mehra, James Urnes, Sr., Mark Hood, and Yohan Lin, "Fast on-Line Actuator Reconfiguration Enabling (FLARE) System", Proceedings of the 2005 AIAA Guidance, Navigation and Control Conference, San Francisco, CA, August 15-18, 2005.
4. J. D. Bošković, S. Bergstrom and R. K. Mehra, "A Multi-Layer Intelligent Loss-of-Control Prevention System (LPS) for Flight Control Applications", Proceedings of the 2005 AIAA Guidance, Navigation and Control Conference, San Francisco, CA, August 15-18, 2005.
5. J. D. Bošković and R. K. Mehra, "A Multiple Model Adaptive Flight Control Scheme for Accommodation of Actuator Failures", AIAA Journal of Guidance, Control & Dynamics, Vol 25, No. 4, pp. 712-724, July-August, 2002.
6. J. D. Bošković and R. K. Mehra, "Intelligent Adaptive Control of a Tailless Advanced Fighter Aircraft under Wing Damage", AIAA Journal of Guidance, Control & Dynamics, Vol. 23, No. 5, pp. 876-884, September-October 2000.
7. M. Brenner, "Aeroservoelastic Modeling and Validation of a Thrust-Vectoring F/A-18 Aircraft", NASA Technical Paper 3647, Sept. 1996.
8. J. Brinker and K. Wise, "Reconfigurable Flight Control of a Tailless Advanced Fighter Aircraft", in Proceedings of the 1998 AIAA Guidance, Navigation and Control Conference, Vol. 1, pp. 75-87, Boston, MA, August 10-12, 1998.
9. Boeing Phantom Works, "Reconfigurable Systems for Tailless Fighter Aircraft - RESTORE (First Draft)", Contract No. F33615-96-C-3612, Scientific and Technical Reports, System Design Report, CDRL Sequence No. A007, St. Louis, Missouri, May 1998.
10. M. Goman and A. Khrabrov, "State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack", J. of Aircraft, Vol.31, No.5, 1994.
11. M. Goman et al. Mathematical description of aircraft's longitudinal aerodynamic characteristics at high angles of attack accounting for dynamic effects of separated flow. TsAGI Preprint.
12. I. M. Gregory, "Dynamic inversion to control large flexible transport aircraft", AIAA-1998-4323, AIAA Guidance, Navigation, and Control Conf., Boston, 1998.
13. I. M. Gregory, "Modified Dynamic Inversion to Control Large Flexible Aircraft - What's Going On?", AIAA-1999-3998, AIAA Guidance, Navigation, and Control Conf., Portland, 1999.
14. I. M. Gregory, "Stability Result for Dynamic Inversion Devised to Control Large Flexible Aircraft", AIAA 2001-4284, AIAA Guidance, Navigation, and Control Conf., Montreal, 2001.
15. Y. Miyazawa, "Flight Control Law and Structural Filter Design for a Flexible Aerospace Vehicle", AIAA-2000-4256, AIAA Guidance, Navigation, and Control Conf., Denver, 2000.
16. M. Moshier, R. Hinrichsen and G. Czarnecki, "Exploring Better Ways to Determine In-Flight Wing Damage: Dynamic Loading Methodologies", Aircraft Survivability, pp. 21-26, Spring 2002.
17. K. S. Narendra and J. Balakrishnan, "Adaptive Control using Multiple Models", IEEE Transactions on Automatic Control, Vol. 42, No. 2, pp. 171-187, February 1997.
18. N. Nguyen, K. Krishnakumar and J. Kaneshige, "Dynamics and Adaptive Control for Stability Recovery of Damaged Asymmetric Aircraft", Proceedings of the AIAA Guidance, Navigation, and Control Conference, August 21-24 2006, Keystone, Colorado.
19. K. Wise, E. Lavretsky, J. Zimmerman, J. Francis, D. Dixon, and B. Whitehead, "Adaptive Flight Control of a Sensor Guided Munition", AIAA GNC Conference, San Fracisco, August 2005.
20. G. Plantanitis, and T. Strganac, "Control of a Nonlinear Wing Section Using Leading- and Trailing-Edge Surfaces", Journal of Guidance, Control & Dynamics, Vol. 27, No. 1, pp. 52-58, January-February 2004.