ARTICLE
Volume 10,Issue 7
30 September 2024
Design and Analysis of Terminal Guidance Law for Kinetic Interceptors based on Pulse Engine
Shixin Li ,
Jia Ma ,
Shuai Yue
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1
School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China,
2
Aerospace System Engineering Shanghai, Shanghai 201100, China,
3
School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China; Shanghai Key Laboratory of Spacecraft Mechanism, Shanghai 201108, China; National Key Laboratory of Space Intelligent Control, Beijing 100048, China,
JERA 2024 , 8(5), 95–108;
https://doi.org/10.26689/jera.v8i5.8400
© 2024 by the Authors. Licensee Whioce Publishing, Singapore. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution 4.0 International License ( https://creativecommons.org/licenses/by/4.0/ )
Abstract
A new terminal guidance law is proposed based on a solid propellant pulse engine and an improved proportional navigation method to address the terminal guidance issue for kinetic interceptors. On this basis, the start-stop curve of the pulse motor during the terminal guidance process is designed, along with its start-up logic. The effectiveness of the proposed guidance strategy is verified through simulation.
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