Damage-Mitigating Control for Wings of Hypersonic Flight Vehicles Based on Modified Prescribed Performance Algorithm

LI Yun-xin; WANG Yu-hui; WU Qing-xian; XU Chao

doi:10.3969/j.issn.1671-637x.2019.08.006

[1] JOYCE P,POMROY J,GRINDLE L.The hyper-X launch vehicle:challenges and design considerations for hypersonic flight testing［C］//AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference,2005.doi:10.2514/6.2005-3333.

[2] WALKER L A,STOUDT W F.Actuator for a g-limiter override:US 4717098［P］.1988-01-05.

[3] MATSUZAKI Y,UEDA T,MIYAZAWA Y,et al.Gust load alleviation of a transport-type wing—Test and analysis［J］.Journal of Aircraft,1989,26(4):322-327.

[4] LORENZO C F.Continuum fatigue damage modeling for critical design,control,and fault prognosis［J］.International Journal of Fatigue,1997,19(10):731.

[5] BECHLIOULIS C P,ROVITHAKIS G A.Robust adaptive control of feedback linearizable MIMO nonlinear systems with prescribed performance［J］.IEEE Transactions on Automatic Control,2008,53(9):2090-2099.

[6] BECHLIOULIS C P,ROVITHAKIS G A.Prescribed performance adaptive control for multi-input multi-output affine in the control nonlinear systems［J］.IEEE Transactions on Automatic Control,2010,55(5):1220-1226.

[7] LEE J H,KO J S,CHUNG S K,et al.Continuous variable structure controller for BLDDSM position control with prescribed tracking performance［J］.IEEE Transactions on Industrial Electronics,1994,41(5):483-491.

[8] KOSTARIGKA A K,ROVITHAKIS G A.Adaptive dyna-mic output feedback neural network control of uncertain MIMO nonlinear systems with prescribed performance［J］.IEEE Transactions on Neural Networks & Learning Systems,2012,23(1):138-149.

[9] DATTOMA V,GIANCANE S,NOBILE R,et al.Fatigue life prediction under variable loading based on a new non-linear continuum damage mechanics model［J］.International Journal of Fatigue,2006,28(2):89-95.

[11] BOLOTIN V V.Prediction of service life for machines and structures［M］.New York:ASME Press,1989.

[12] RAY A,WU M K.Damage-mitigating control of space propulsion systems for high performance and extended life［R］.Washington:NASA Contractor Report 194470, 1994.

[15] GUO Z Y,CHANG J,GUO J G,et al.Adaptive twisting sliding mode algorithm for hypersonic reentry vehicle attitude control based on finite-time observer［J］.ISA Transactions,2018,77:20-29.

[17] RAY A,DAI X W,WU M K,et al.Damage-mitigating control of a reusable rocket engine［J］.Journal of Propulsion and Power,1994,10(2):225-234.