Adaptive terminal sliding mode control for hypersonic flight vehicles with strictly lower convex function based nonlinear disturbance observer. (November 2017)

• Record Type: Journal Article
• Authors: Wu, Yun-jie; Zuo, Jing-xing; Sun, Liang-hua
• Is Part Of: ISA transactions. Volume 71:Part 2(2017)
• Page Start: 215
• Page End: 226
• Publication Date: 2017-11
• Subjects: HFV -- SDOB -- Terminal sliding mode control -- Adaptive law; Engineering instruments -- Periodicals; Engineering instruments; Periodicals; Electronic journals; 629.805
• DOI: 10.1016/j.isatra.2017.08.008
• Languages: English
• ISSNs: 0019-0578

Abstract

Abstract: In this paper, the altitude and velocity tracking control of a generic hypersonic flight vehicle (HFV) is considered. A novel adaptive terminal sliding mode controller (ATSMC) with strictly lower convex function based nonlinear disturbance observer (SDOB) is proposed for the longitudinal dynamics of HFV in presence of both parametric uncertainties and external disturbances. First, for the sake of enhancing the anti-interference capability, SDOB is presented to estimate and compensate the equivalent disturbances by introducing a strictly lower convex function. Next, the SDOB based ATSMC (SDOB-ATSMC) is proposed to guarantee the system outputs track the reference trajectory. Then, stability of the proposed control scheme is analyzed by the Lyapunov function method. Compared with other HFV control approaches, key novelties of SDOB-ATSMC are that a novel SDOB is proposed and drawn into the (virtual) control laws to compensate the disturbances and that several adaptive laws are used to deal with the differential explosion problem. Finally, it is illustrated by the simulation results that the new method exhibits an excellent robustness and a better disturbance rejection performance than the convention approach. Highlights: The strict feedback formed longitudinal model of a generic HFV is described. A novel strictly lower convex function based nonlinear disturbance observer is proposed. Adaptive laws are utilized to simplify the tedious and complicated differential operation. The composite control scheme guarantees that the tracking error converges to a neighborhood around the origin.