首页|基于综合优化函数的中制导段弹道规划

基于综合优化函数的中制导段弹道规划

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为合理规划制导炮弹中制导段的滑翔弹道,构建了综合优化函数,并将其作为弹道规划的性能指标.相比于传统性能指标,所提函数综合考虑了炮弹在滑翔飞行时的能量损失与机动效率,解决了传统性能指标过于片面等问题.为验证其有效性与优越性,着重分析了其取值对滑翔弹道的影响,并利用hp-自适应拉道伪谱法对弹道规划问题进行求解.结果表明,以综合优化函数作为性能指标,可以大大提高制导炮弹的末端速度以及机动能力,有利于提高炮弹的命中精度与毁伤效能.此外,综合优化函数也可与传统性能指标相结合,构建复合型优化指标,进一步扩大其应用范围.
Trajectory planning of medium guidance based on comprehensive optimization function
In order to plan the medium glide trajectory of guided projectile,the comprehensive optimization function is constructed and used as a performance indicator for trajectory planning.Compared with the traditional performance index,the function comprehensively reflects the energy loss and maneuvering efficiency of the projectile in gliding flight,and solves the problem that the traditional performance indicator is too one-sided.To verify the effectiveness and superiority of the function,the influence of its value on the gliding trajectory is analyzed,and the problem of trajectory planning is solved based on the hp-adaptive radau pseudospectral method.The results show that taking the comprehensive optimization function as the performance index can greatly improve the terminal velocity and maneuverability of the guided projectile,which is conducive to improve the hit accuracy and damage efficiency of the projectile.In addition,the comprehensive optimization function can also be combined with the traditional performance index to construct composite optimization index,further expanding its application scope.

guided projectilemedium guidancetrajectory planningenergy loss ratemaneuver ef-ficiencycomprehensive optimization functionradau pseudospectral method

郭佳晖、蒋滨安、殷庆虎、张航

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中国人民解放军陆军炮兵防空兵学院,合肥 230031

中国人民解放军91991部队,舟山 316000

制导炮弹 中制导 弹道规划 能量损失率 机动效率 综合优化函数 拉道伪谱法

2024

战术导弹技术
中国航天科工飞航技术研究院(中国航天科工集团第三研究院)

战术导弹技术

CSTPCD北大核心
影响因子:0.304
ISSN:1009-1300
年,卷(期):2024.(3)