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Publishing Language: Chinese

Three-dimensional cooperative guidance with field-of-view constraints based on event-triggered mechanism

Zhichuan HE1,2Jiang WANG1,2Shipeng FAN1,2( )Peng WANG1,2Miao HOU1,2
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
China-UAE Belt and Road Joint Laboratory on Intelligent Unmanned System, Beijing Institute of Technology, Beijing 100081, China
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Abstract

To meet the requirement for simultaneousness of multiple anti-ship missiles in attacking a ship target, this paper investigates the time-cooperative guidance problem with the event-triggered control method by considering the seeker’s field-of-view constraint. A three-dimensional time-cooperative guidance law consisting of the three-dimensional proportional navigation guidance law and an event-triggered bias term is proposed based on the three-dimensional coupled nonlinear model, and the event- event-triggering conditions are also provided. The bias term utilizes a nonlinear function to ensure that the velocity lead angle is bounded to satisfy the seeker’s field-of-view constraint and enables the impact times of multiple missiles can synchronize by means of a distributed event-triggered consensus protocol, thus reducing the frequency of cooperative control system updates and communication resource consumption. Using the Lyapunov theory, the convergence of the proposed distributed cooperative guidance law is demonstrated to have no Zeno behavior. Finally, numerical simulations are conducted to verify the effectiveness and robustness of the proposed three-dimensional cooperative guidance law.

CLC number: V448 Document code: A

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Acta Aeronautica et Astronautica Sinica
Article number: 328687

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Cite this article:
HE Z, WANG J, FAN S, et al. Three-dimensional cooperative guidance with field-of-view constraints based on event-triggered mechanism. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 328687. https://doi.org/10.7527/S1000-6893.2023.28687

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Received: 13 March 2023
Revised: 18 April 2023
Accepted: 01 June 2023
Published: 20 September 2023
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica