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Integrated Reconfigurable Aero-Propulsion (IRAP) Control for Improved Fault Tolerance
Technical Paper
2013-01-2255
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
In this paper we present results of a study of an integrated aero-propulsion flight control system. The resulting problem is that of controlling the system in which actuators operate on different time scales. This is a difficult problem since the control strategy needs to balance between not using the slow actuator at all, and slowing down the overall system to the time scale of the slow actuator. In the case of aero-propulsion control design for F/A-18 aircraft, the part of the control derivative matrix associated with engines is not full rank so not all states of interest can be simultaneously forced to track the commands. A control strategy that takes this constraint into account has been developed. The proposed IRAP approach is illustrated through simulation of F/A-18 aircraft dynamics under flight-critical control effector failures.
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Authors
Citation
Boskovic, J., Jackson, J., and Mehra, R., "Integrated Reconfigurable Aero-Propulsion (IRAP) Control for Improved Fault Tolerance," SAE Technical Paper 2013-01-2255, 2013, https://doi.org/10.4271/2013-01-2255.Also In
References
- Ahmed-Zaid F. , Ioannou P. , Gousman K. and Rooney R. Accommodation of Failures in the F-16 Aircraft using Adaptive Control IEEE Control Systems Magazine 11 1 73 78 January 1991
- Bodson M. and Groszkiewicz J. Multivariable Adaptive Algorithms for Reconfigurable Flight Control IEEE Transactions on Control Systems Technology 5 2 217 229 March 1997
- Boeing Phantom Works Reconfigurable Systems for Tailless Fighter Aircraft - RESTORE Contract No. F33615-96-C-3612, Scientific and Technical Reports No. A007 St. Louis, Mo May 1998
- Bošković J. D. , Knoebel N. and Redding J. Integrated Damage Adaptive Control System (IDACS) Final Report under NASA Langley Phase II SBIR, Contract No. NNL07AA02C May 2009
- Bošković J. D. and Knoebel N. Integrated Reconfigurable Aero-Propulsion (IRAP) Control for Improved Flight Safety of Commercial Aircraft Final Report for NASA Ames Phase I SBIR, Contract No. NNX08CA51P July 2008
- Bošković J. D. , Jackson J. , Redding J. and Mehra R. K. Onboard Autonomy Through Integration of Health Management and Control Reconfiguration Final Report for NASA Ames Phase II SBIR, Contract No. NNA06AA04C March 2008
- Bošković J. D. and Mehra R. K. A Multiple Model-based Decentralized System for Accommodation of Failures in Second-Order Flight Control Actuators Proceedings of the 2006 American Control Conference Minneapolis, MN June 14 16 2006
- Bošković J. D. and Mehra R. K. Robust Integrated Flight Control Design Under Failures, Damage and State-Dependent Disturbances AIAA Journal of Guidance, Control & Dynamics 28 5 902 917 September October 2005
- Bošković J. D. , Prasanth R. and Mehra R. K. Retrofit Reconfigurable Flight Control Proceedings of the 2005 AIAA Guidance, Navigation and Control Conference San Francisco, CA August 15 18 2005
- Bošković J. D. , Bergstrom S. and Mehra R. K. 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
- Bošković J. D. , Bergstrom S. E. , Mehra R. K. , Urnes J. Sr. , Hood M. , and Lin Y. 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
- Prasanth R. K. and Bošković J. D. Stability Analysis and Design of Optimal One Step Ahead Controllers Proceedings of the 2005 AIAA Guidance, Navigation and Control Conference San Francisco, CA August 15 18 2005
- Bošković J. D. and Mehra R. K. Failure Detection, Identification and Reconfiguration in Flight Control Fault Diagnosis and Fault Tolerance for Mechatronic Systems , Recent Advances Series: Springer Tracts in Advanced Robotics 1 Caccavale F. and Villani L. Springer Verlag NY 2002
- Bošković J. D. and Mehra R. K. A Multiple Model Adaptive Flight Control Scheme for Accommodation of Actuator Failures AIAA Journal of Guidance, Control & Dynamics 25 4 712 724 July August 2002
- Bošković J. D. and Mehra R. K. Aircraft Prognostics and Health Management (PHM) and Adaptive Reconfigurable Control (ARC) System NASA DFRC Phase II SBIR Final Report, Contract No: NAS4-02017 March 2004
- Bošković J. D. and Mehra R. K. Intelligent Adaptive Control of a Tailless Advanced Fighter Aircraft under Wing Damage AIAA Journal of Guidance, Control & Dynamics 23 5 876 884 September October 2000
- Bošković J. D. , Li S.-M. and Mehra R. K. Evaluation of the Properties of a Multiple-Model Reconfigurable Flight Controller on a 6 DOF Simulation Proceedings of the 2000 AIAA Guidance, Navigation and Control (GNC) Conference Denver, CO August 2000
- Brinker J. and Wise K. Reconfigurable Flight Control of a Tailless Advanced Fighter Aircraft Proceedings of the 1998 AIAA Guidance, Navigation and Control Conference 1 75 87 Boston, MA August 10 12 1998
- Burcham F. W. , Burken J. , and Maine T. Flight Testing a Propulsion-Controlled Aircraft Emergency Flight Control System on an F-15 Airplane NASA Technical Memorandum 4590 Dryden Flight Research Center Edwards, CA June 1994
- Burcham F. , Maine T. , Burken J. and Bull J. Using Engine Thrust for Emergency Flight Control: MD-11 and B-747 Results NASA Technical Memorandum 206552 Dryden Flight Research Center Edwards, CA May 1998
- Calise A. , Lee S. and Sharma M. Direct Adaptive Reconfigurable Control of a Tailless Fighter Aircraft Proceedings of the 1998 AIAA Guidance, Navigation and Control Conference 1 88 97 Boston, MA August 10 12 1998
- Chandler P. , Pachter M. and Mears M. System Identification for Adaptive and Reconfigurable Control Journal of Guidance, Control & Dynamics 18 3 516 524 May June 1995
- Narendra K. S. and Annaswamy A. M. Stable Adaptive Systems Prentice Hall Inc. Englewood Cliffs, New Jersey 1988
- Krstić M. , Kanellakopoulos I. , and Kokotović P. Nonlinear and Adaptive Control Design John Wiley & Sons 1995
- Subrahmanyam M. H ∞ Design of F/A-18A Automatic Carrier Landing System Journal of Guidance, Control, and Dynamics 17 1 187 191 1994
- Wise K. , Lavretsky E. , Zimmerman J. , Francis J. , Dixon D. and Whitehead B. Adaptive Flight Control of a Sensor Guided Munition AIAA Paper AIAA-2005-6385 2005
- Wise K. Boeing/DARPA UCAV Program Highlights Boeing Phantom Works St. Louis, MO January 2000
- Narendra K. S. and Balakrishnan J. Adaptive Control using Multiple Models IEEE Transactions on Automatic Control 42 2 171 187 February 1997