Abstract：This study delves into the design methodology for typical maneuvering trajectories to enhance the maneuver
penetration capability of hypersonic glide vehicles. Firstly, a high-precision altitude-velocity analytical solution was
derived and used as the foundation for longitudinal trajectory designing. Secondly, based on the altitude and crossrange
analytical solutions, longitudinal and lateral maneuver modes were devised to execute longitudinal skip and lateral
weaving maneuvers. The effects of these modes on the vehicle's overload were analyzed, providing a basis for the
choice of maneuver mode in the practical penetration. By meticulously designing the amplitude, frequency, and phase
of trajectories in both longitudinal and lateral maneuver modes, spatial spiral and pendulum maneuvers were acquired.
Finally, the effectiveness of the maneuver trajectory design method was simulated and verified, presenting high
accuracy and meeting penetration requirements.
刘政卓, 王伟, 张勃, 贺祥, 闫杰. 基于解析解的高超声速滑翔飞行器的机动弹道设计[J]. 空天防御, 2024, 7(3): 102-110.
LIU Zhengzhuo, WANG Wei, ZHANG Bo, HE Xiang, YAN Jie. Maneuvering Trajectory Design for Hypersonic Gliding
Vehicles Based on Analytical Solutions. Air & Space Defense, 2024, 7(3): 102-110.
