Robust Gain-Scheduling Controller for Airbreathing Hypersonic Flight Vehicle

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This paper addresses issues related to robust control for an airbreathing hypersonic flight vehicle. Owing to aero-propulsion couplings caused by the unique structure shape, the model of the vehicle is greatly nonlinear and complex, which presents an enormous technical challenge for control. The nonlinear model is transformed into a linear fractional transformation (LFT) model, and a robust gain-scheduling controller based on linear parameter-varying control (LPV) with full block multipliers is obtained. Simulations illustrate great improvements of the dynamic performance in closed-loop system.

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1624-1630

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December 2014

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] Matthew Kuipers, Majdedin Mirmirani, Petros Ioannou, Ying Huo, Adaptive Control of an Aeroelastic AirbreathingHypersonic Cruise Vehicle, AIAA Guidance, Navigation and Control Conference and Exhibit, 20-23 August 2007, Hilton Head, South Carolina.

DOI: 10.2514/6.2007-6326

Google Scholar

[2] Ying Huo, Majdedin Mirmirani, Petros Ioannou, Matthew Kuipers, Altitude and Velocity Tracking Control forAn Airbreathing Hypersonic Cruise Vehicle, AIAA Guidance, Navigation, and Control Conference and Exhibit, 21-24 August 2006, Keystone, Colorado.

DOI: 10.2514/6.2006-6695

Google Scholar

[3] Andrew D. Clark, Maj Dean Mirmirani, Chivey Wu, Sangbum Choi, An Aero-Propulsion Integrated Elastic Model of a GenericAirbreathing Hypersonic Vehicle, AIAA Guidance, Navigation, and Control Conference and Exhibit, 21-24 August 2006, Keystone, Colorado.

DOI: 10.2514/6.2006-6560

Google Scholar

[4] Andrew Clark, Chivey Wu, Maj Mirmirani, Sangbum Choi, Development of an Airframe-Propulsion Integrated GenericHypersonic Vehicle Model, 44th AIAA Aerospace Sciences Meeting and Exhibit, 9-12 January 2006, Reno, Nevada.

DOI: 10.2514/6.2006-218

Google Scholar

[5] Maj Mirmirani, Matthew Kuipers, Jason Levin, Andrew D. Clark, Flight DynamicCharacteristics of a Scramjet-Powered Generic Hypersonic Vehicle, 2009 American Control Conference, Hyatt Regency Riverfront, St. Louis, MO, USA, June 10-12, (2009).

DOI: 10.1109/acc.2009.5160500

Google Scholar

[6] Maj Mirmirani, Chivey Wu, Andrew Clark, Sangbum Choi, Richard Colgren, Modeling for Control of a Generic Airbreathing HypersonicVehicle, AIAA Guidance, Navigation, and Control Conference and Exhibit, 15 - 18 August 2005, San Francisco, California.

DOI: 10.2514/6.2005-6256

Google Scholar

[7] C. W. Scherer, LPV control and full block multipliers, Automatica. 37 (2001) 361-375.

DOI: 10.1016/s0005-1098(00)00176-x

Google Scholar

[8] Jianqiao Yu, Guanchen Luo, Wentao Yin, Missile robust gain scheduling autopilot design using full block multipliers, Journal of Systems Engineering and Electronics. 21 (2010) 883-891.

DOI: 10.3969/j.issn.1004-4132.2010.05.024

Google Scholar

[9] Xianlin Huang, Dongming Ge, Robust Linear Parameter-Varying Control for Longitudinal Maneuvering Flight of Air-Breathing Hypersonic Vehicle, Journal of Astronautics. 31 (2010) 1789-1797. (In Chinese).

DOI: 10.1109/icca.2010.5524121

Google Scholar

[10] Boyd S, Ghaoui L E, Feron E, et al, Linear Matrix Ineualities in System and Control theory, (1994).

Google Scholar