| Citation: | ZHANG S，SONG T L，JIAO W，et al. Cooperative guidance method with interception time constraint[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：1956-1963 （in Chinese） doi: 10.13700/j.bh.1001-5965.2021.0569
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To address the problem of multi-aircraft cooperative interception of maneuvering targets, a cooperative guidance method considering interception time constraints is proposed based on the finite-time sliding mode control method and consistency theory. Based on the relative kinematics and dynamics, a cooperative interception model considering interception time and angle constraints is established. Based on the sliding mode control theory and super-twisting control algorithm, the coordinate guidance laws in line-of-sight direction and line-of-sight normal direction are designed to ensure that the interception time of each aircraft converges uniformly within the finite time and that the interception angle converges to the expected value. Based on the consistency theory, the finite-time consistent convergence performance of the proposed guidance method is demonstrated. The simulation results show that all the aircrafts can intercept targets simultaneously at the desired intercept angle, which verifies the effectiveness of the proposed method.
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