ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Prescribed performance guidance law with field-of-view and impact angle constraints
Received date: 2023-03-30
Revised date: 2023-04-24
Accepted date: 2023-05-15
Online published: 2023-05-17
Supported by
National Natural Science Foundation of China(12002370)
To address the problem of guided missiles against non-maneuvering targets， a prescribed performance guidance law with seeker Field-of-View （FOV） and impact angle constraints is proposed. Firstly， a prescribed time performance function is designed to enable direct setting of the convergence time， the upper and lower bounds of the tracking error. Through error transformation， the tracking error control problem under performance boundary constraints is transformed into an unconstrained stable control problem. Secondly， the guidance law is designed as the sum of a pure proportional guidance term and a bias term. The bias term is derived based on the optimal error dynamics method to control the transformation error within a bound， ensure that the tracking error consistently converges within the performance boundary， and ultimately achieve terminal impact angle constraint. Furthermore， based on the proposed guidance law， the in-depth analysis of the parameters in the performance function is conducted， and reasonable parameters ranges are provided. Moreover， considering seeker FOV limitation and moving target scenario， an auxiliary function and the predicted interception point concept are introduced to improve the guidance law respectively， which realize the FOV constraint and the extension of proposed law against moving target. Finally， the effectiveness of the proposed guidance law is verified through numerical simulations.
Haojian LI , Yuanhe LIU , Yangang LIANG , Kebo LI . Prescribed performance guidance law with field-of-view and impact angle constraints[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023 , 44(15) : 528764 -528764 . DOI: 10.7527/S1000-6893.2023.28764
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