Profile-tracking-based gain-varying backstepping guidance law for maneuvering target interception with input

Jingliang Sun1, Mengmeng Wang2, Zihan Wang2

  • 1School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China; Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China; Beijing Institute of Technology Chongqing Innovation Center, Chongqing 401135, China.

ISA Transactions
|November 18, 2025
PubMed
Summary

This study introduces a novel guidance law for missiles to intercept maneuvering targets, ensuring a precise impact angle even with system limitations. The developed method offers effective trajectory control and guaranteed stability.

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