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Input-and-measurement event-triggered control for flexible air-breathing hypersonic vehicles with asymmetric partial-state constraints

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Abstract

In this paper, an input-and-measurement event-triggered control scheme considering asymmetric partial-state constraints is proposed for flexible air-breathing hypersonic vehicles (FAHV) subject to lumped disturbances and limited resources. To realize a precise disturbance rejection with decreased communication burden in sensor-to-control channels, intermittent measurement-based extended state observers using switching threshold samplers are developed in altitude and velocity subsystems, while the quantitative relationship between the upper bounds of observation errors and the design parameters of switching triggering mechanism is derived. Subsequently, to ensure the angle of attack (AoA) well within the allowable operational region and simultaneously achieve a reference tracking with expected characteristic, asymmetric constraints imposed on partial states including AoA, velocity, and altitude are embedded in design process, while a one-to-one nonlinear mapping is designed to avoid the violation of state constraint of AoA without enforcing feasibility conditions on virtual control laws, and a modified prescribed performance control is constructed to govern the output constraints of velocity and altitude, releasing the demand on the precise knowledge of initial states. Next, to maintain the resources occupation (energy and communication in controller-to-actuator channel) at low levels and ensure a desirable tracking precision, robust control laws based on switching event-triggered mechanisms are designed for FAHV to circumvent Zeno phenomena and compensate for the sampling error induced by event-triggered conditions. The simulation results and comparisons validate the effectiveness of the proposed scheme.

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Acknowledgements

This research has been supported in part by National Natural Science Foundation of China under grant 61803348, State Key Laboratory of Deep Buried Target Damage under grant DXMBJJ2019-02, Scientific and Technological Innovation Programs of Higher Education Institutions in Shanxi under grant 2020L0266, Shanxi Province Science Foundation for Youths under grant 201701D221123, Youth Academic Leader Program of North University of China under grant QX201803, Program for the Innovative Talents of Higher Education Institutions of Shanxi, and Shanxi “1331 Project” Key Subjects Construction (1331KSC).

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Authors and Affiliations

  1. Key Laboratory of Instrumentation Science and Dynamic Measurement, Ministry of Education, North University of China, Taiyuan, 030051, China

    Xingling Shao, Yi Shi & Wendong Zhang

  2. National Key Laboratory for Electronic Measurement Technology, School of Instrument and Electronics, North University of China, Taiyuan, 030051, China

    Xingling Shao, Yi Shi & Wendong Zhang

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  1. Xingling Shao
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  2. Yi Shi
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Correspondence to Xingling Shao.

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Shao, X., Shi, Y. & Zhang, W. Input-and-measurement event-triggered control for flexible air-breathing hypersonic vehicles with asymmetric partial-state constraints. Nonlinear Dyn 102, 163–183 (2020). https://doi.org/10.1007/s11071-020-05942-7

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