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Dec. 2022
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Jinglei Ren, Zhenya Wang, Feng Fang. Model Predictive Control Based Defensive Guidance Law in Three-Body Engagement[J]. JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2022, 31(6): 559-569. doi: 10.15918/j.jbit1004-0579.2021.106
Citation: Jinglei Ren, Zhenya Wang, Feng Fang. Model Predictive Control Based Defensive Guidance Law in Three-Body Engagement[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2022, 31(6): 559-569.doi:10.15918/j.jbit1004-0579.2021.106
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Model Predictive Control Based Defensive Guidance Law in Three-Body Engagement

doi:10.15918/j.jbit1004-0579.2021.106
  • 1.

    China Academy of Launch Vehicle Technology, Beijing 100076, China

  • 2.

    School of Automation, Hangzhou Dianzi University, Zhejiang 310018, China

Funds:This work was supported by the National Natural Science Foundation of China(No. 61673146) and Zhejiang Provincial University Research Foundation(GK209907299001-021).
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  • Author Bio:

    Jinglei Renis currently an engineer with China Academy of Launch Vehicle Technology. His research interests include missile guidance and control

    Zhenya Wangis a researcher with China Academy of Launch Vehicle Technology. His research interests include fault diagnosis and intelligent decision

    Feng Fangis currently an Assistant Professor with Hangzhou Dianzi University. His current research interests include cooperative guidance and control

  • Corresponding author:oyowzy@163.com
  • Received Date:2022-01-05
  • Rev Recd Date:2022-05-17
  • Accepted Date:2022-07-08
  • Publish Date:2022-12-25
    Abstract
  • Model predictive control (MPC) has been widely used in process industry, but its applications to missile guidance law are relatively rare. In this paper, MPC is introduced to design defensive guidance law in a three-body engagement, where a defending missile (i.e., defender) is employed to protect a target aircraft from an attacking missile. Based on nonlinear kinematic equations, an explicit linear discrete-time model is derived as the predictive model. Then the defensive guidance problem is formulated as a quadratic programming problem, and a fast algorithm for the MPC guidance law is developed. The advantages of the MPC guidance law include the applicability to scenarios with unknown guidance strategy of attacking missile, nonlinear kinematics and multiple constraints. Another key feature is that the proposed approach does not require alteration in the target maneuver. Simulation results show that the MPC guidance law works well and can meet real-time requirements.
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