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.
国家科技期刊平台
NSTL
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