Abstract In this study, hypersonic vehicle (HV) tracking control in the presence of uncertainties and external disturbance is investigated. As the exact bounds of uncertainties and disturbances are usually unknown during flight, a disturbance observer (DOB)-based gain adaptation high-order sliding mode control (HOSMC) method is proposed for HVs. To mitigate the chattering effect while maintaining strong robustness, a method combining the advantages of the DOB and gain adaptation is introduced into the HOSMC. The DOB is employed to estimate and reject the uncertainties and external disturbance. Additionally, an adaptive control law is developed to compensate for estimation errors. By combining the DOB and the adaptive HOSMC, the unnecessarily large gain for maintaining robustness is reduced; thus, the chattering is mitigated. The effectiveness of the proposed control method is validated via simulation, in which a strong robustness, high tracking performance, and reduced chattering effect are achieved under uncertainties and external disturbance.
Disturbance observer-based gain adaptation high-order sliding mode control of hypersonic vehicles
Xiaomeng Yin,Bo Wang,Lei Liu,Yongji Wang
Published 2019 in Aerospace Science and Technology
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- Publication year
2019
- Venue
Aerospace Science and Technology
- Publication date
2019-06-01
- Fields of study
Computer Science, Engineering
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