| Citation: | YIN Q L，CHEN Q，WANG Z Y，et al. Trajectory programming method of gliding-guided projectiles for penetration[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3151-3161 （in Chinese） doi: 10.13700/j.bh.1001-5965.2023.0049
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Aiming at the problem of gliding-guided projectile penetration schemes in inevitable threat areas, mathematical models of the enemy’s defense are established from the perspective of quantifying the threat value. Based on the model, a cost function with the lowest comprehensive threat value in the whole process is designed. To accomplish the best possible matching of the initial trajectory inclination, deflection angle, rocket ignition time, gliding start time, and other parameters over the course of the flight, a multi-stage full trajectory planning model is created. Then, the hp adaptive pseudo-spectral method is used to transform the optimal control problem into a nonlinear programming problem. The evading effect of the projectile on target defense is verified by simulation, and the factors affecting the effectiveness are analyzed. The proposed method’s advantages over conventional trajectory programming techniques are also examined.
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