Guidance law against maneuvering targets with intercept angle constraint.
This study explores the guidance law against maneuvering targets with the intercept angle constraint. The limitation of the traditional guidance law, which simply treats the unknown target acceleration as zero, has been analyzed. To reduce this limitation, a linear extended state observer is constructed to estimate the acceleration of the maneuvering target to enhance the tracking performance of the desired intercept angle. Furthermore, a nonsingular terminal sliding mode control scheme is adopted to design the sliding surface, which is able to avoid the singularity in the terminal phase of guidance. Simulation results have demonstrated that the proposed guidance law outperforms the traditional guidance law in the sense that more accurate intercept angle can be achieved.
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics & Astronautics, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics & Astronautics, Beijing 100191, China. Electronic address: 15210985746@163.com.
Shaofeng
S
Xiong
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics & Astronautics, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics & Astronautics, Beijing 100191, China.
Weihong
W
Wang
Beijing Aerospace Automatic Control Institute, Beijing 100854, China; National Key Laboratory of Science and Technology on Aerospace Intelligence Control, Beijing 100854, China.
Xiaodong
X
Liu
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics & Astronautics, Beijing 100191, China; Science and Technology on Aircraft Control Laboratory, Beijing University of Aeronautics & Astronautics, Beijing 100191, China.
Sen
S
Wang
Department of Automation, Nankai University, Tianjin 300071, China.
Zengqiang
Z
Chen
Extended state observer; Intercept angle constraint; Maneuvering target; Nonlinear guidance law; Sliding mode control