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Fault-tolerant control of hypersonic vehicles based on fast fault observer under actuator gain loss fault or stuck fault

Published online by Cambridge University Press:  09 March 2020

P. Zhu Open the ORCID record for P. Zhu [Opens in a new window] ,
J. Jiang  and
C. Yu
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Abstract

This paper proposes a fault-tolerant control (FTC) method based on fast fault observer (FFO) to solve the problem of actuator gain loss fault and stuck fault for hypersonic vehicles. Firstly, an input-output feedback linearisation model is presented that considers parametric uncertainties, control input saturation, disturbances and actuator faults. Secondly, the above factors are defined as an integrated fault item, and an improved fast fault observer is designed to estimate the integrated fault in real time. Finally, the fault-tolerant controller is constructed based on the sliding mode and fault estimation. In case of unknown faults, the effects of gain loss fault or stuck fault happen on elevators and the engine can be quickly processed, Also, the asymptotically stable tracking of the flight output reference command is completed to achieve fault-tolerant control. The final simulation experiment verifies the effectiveness of the proposed method.

Keywords

Hypersonic vehicleActuator gain loss faultStuck faultFast fault observerFault-tolerant control
Type
Research Article
Information
The Aeronautical Journal , Volume 124 , Issue 1278 , August 2020 , pp. 1190 - 1207
Copyright
© The Author(s) 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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References

REFERENCES

Voland, R.T., Huebner, L.D. and Mcclinton, C.R.X-43A hypersonic vehicle technology development, Acta Astronaut, 2009, 59, (1–5), pp 181–191.CrossRefGoogle Scholar
Xu, B. and Shi, Z.K.An overview on flight dynamics and control approaches for hypersonic vehicles, China Inf Sci, 2015, 58, (7), pp 1–19.CrossRefGoogle Scholar
Friedmann, P. and Mcnamara, J. Aeroelastic and Aerothermoelastic Analysis of Hypersonic Vehicles: Current Status and Future Trends, AIAA Paper 2007-2013, 2007.CrossRefGoogle Scholar
Shen, Q., Jiang, B. and Cocquempot, V.Fault-tolerant control for T-S fuzzy systems with application to near-space hypersonic vehicle with actuator faults, IEEE Trans. Fuzzy Syst., 2012, 20, (4), pp 652–665.CrossRefGoogle Scholar
Chen, F., Wang, Z., Tao, G., et al.Robust adaptive fault tolerant control for hypersonic flight vehicles with multiple faults, J Aerosp Eng, 2015, 28, (4), pp 0401–4111.10.1061/(ASCE)AS.1943-5525.0000449CrossRefGoogle Scholar
He, J., Qi, R., Jiang, B., et al.Adaptive output feedback fault-tolerant control design for hypersonic flight vehicles. J Franklin Inst, 2015, 352, (5), pp 1811–1835.CrossRefGoogle Scholar
Niu, J., Chen, F. and Tao, G.Nonlinear fuzzy fault-tolerant control of hypersonic flight vehicle with parametric uncertainty and actuator fault, Nonlinear Dyn, 2018, 92, (3), pp 1299–1315.CrossRefGoogle Scholar
Wang, J., Zong, Q., He, X., et al.Adaptive finite-time control for a flexible hypersonic vehicle with actuator fault, Math Prob Eng, 2013, (1), pp 1–10.Google Scholar
Askari, M.R., Shahrokhi, M. and Talkhoncheh, M.K.Observer-based adaptive fuzzy controller for nonlinear systems with unknown control directions and input saturation, Fuzzy Sets Syst, 2016, 314.Google Scholar
Mu, L., Li, L., Yu, X., et al.Observer-based fault-tolerant control of hypersonic scramjet vehicles in the presence of actuator faults and saturation, Int J Robust Nonlinear Cont, 2017.Google Scholar
Groves, K., Serrani, A., Yurkovich, S., et al. Anti-windup control for an air-breathing hypersonic vehicle model, 2005.CrossRefGoogle Scholar
Gibson, T.E., Crespo, L.G., Annaswamy, A.M. Adaptive control of hypersonic vehicles in the presence of modeling uncertainties, American Control Conference, 2009, pp 3178–3183.CrossRefGoogle Scholar
Sun, H., Li, S., Sun, C.Adaptive fault-tolerant controller design for airbreathing hypersonic vehicle with input saturation, J Syst Eng Electron, 2013, 24, (3), pp 488–499.10.1109/JSEE.2013.00057CrossRefGoogle Scholar
Bolender, M.A. An overview on dynamics and controls modelling of hypersonic vehicles, Proceedings of the American Control Conference (ACC ’09), St. Louis, MO, USA, June 2009, pp 2507–2512.CrossRefGoogle Scholar
Sigthorsson, D.O. and Serrani, A. Development of linear parameter-varying models of hypersonic air-breathing vehicles, Proceedings of the AIAA Guidance, Navigation, and Control Conference and Exhibit, Chicago, Ill, USA, August 2009.CrossRefGoogle Scholar
Xu, H.J., Mirmirani, M.D., Ioannou, P.A.Adaptive sliding mode control design for a hypersonic flight vehicle. J Guid Control Dyn, 2014, 27, pp 829–838.CrossRefGoogle Scholar
Levant, A. and Livne, M.Exact differentiation of signals with unbounded higher derivatives, IEEE Transactions on Automatic Control, 2012, 57, (4), pp 1076–1080.CrossRefGoogle Scholar