摘要
基于摄动制导导引律研发出一种适合一体化PGK硬件的制导控制算法,改善导弹对机动目标的截获能力,强化制导与控制之间的协调匹配,实现高精度制导。比较了单纯滤波和实时计算导引系数的抗干扰措施,并在仿真和试验测试中证明了控制算法的有效性及实时计算导引系数方法的优越性。
Based on the perturbation guidance law,a guidance control algorithm suitable for integrated PGK hardware is proposed,which improves the interception capability of the missile for the maneuvering target,strengthens the coordination and matching between guidance and control and achieves high-precision guidance. The anti-jamming measures of simple filtering and real-time calculation of guiding coefficients are compared,and the effectiveness of the control algorithm and the superiority of real-time calculation of guiding coefficients are proven in simulation and experimental tests.
作者
彭俊然
陈庆
邓健辉
杨世武
李闯
Peng Junran;Chen Qing;Deng Jianhui;Yang Shiwu;Li Chuang(Huazhong University of Science and Technology,Wuhan 430074,China;China Aerospace Science and Technology Group Fenghuo Machinery Factory,Chengdu 611130,China)
出处
《航天控制》
CSCD
北大核心
2019年第4期27-34,共8页
Aerospace Control
基金
航天科技创新基金项目(KJCX-JT-1601)
关键词
精确制导组件
一体化
控制系统
摄动制导
实弹试验
Precision guidance kit
Integration
Control system
Perturbation guidance
Live ammunition test
