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.
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.
Area of Science:
- Aerospace Engineering
- Control Systems Theory
- Robotics
Background:
- Guidance systems face challenges with maneuvering targets and input saturation.
- Achieving precise impact angle control is critical for interception effectiveness.
Purpose of the Study:
- To develop a profile-tracking-based, gain-varying backstepping guidance law.
- To address impact angle constraints for maneuvering targets with input saturation.
Main Methods:
- Formulated a range-elapsed-based polynomial function for reference line-of-sight angle profile.
- Developed a gain-varying finite-time constrained backstepping guidance law.
- Designed a tracking-error-based varying gain to counter target maneuvers.
Main Results:
- The reference profile can be determined analytically without numerical optimization.
- The proposed guidance law effectively tracks the designed profile.
- Theoretical guarantees for the closed-loop system stability were established.
Conclusions:
- The developed guidance law is effective for impact angle constrained guidance.
- Comparative simulations confirm the method's advantages over existing approaches.
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