| Citation: | ZHANG K Q，ZHOU X F，MEN X H，et al. Three-dimensional integrated guidance and control design with fixed-time convergence[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（4）：842-852 （in Chinese） doi: 10.13700/j.bh.1001-5965.2021.0360
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This paper proposes a three-dimensional integrated design method for missile guidance and control with fixed-time convergence to address the issues of impact angle constraints, state constraints, and control constraints. A three-channel fully coupled design model of guidance and control system with impact angle constraints is constructed, and the unknown disturbances in the integrated design model are estimated and compensated by a fixed-time convergent sliding mode disturbance observer. Based on the fixed-time stability theory, terminal sliding mode control and backstepping control method, the integrated design of the guidance and control system is carried out, and the second-order instruction filter is used to restrict the system states and control instructions. The fixed-time convergence property of the integrated algorithm is proved, and the specific convergence time expression is given. The effectiveness and superiority of the integrated guidance and control law are verified by six degrees of freedom simulation of the missile.
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