航空兵器2024，Vol.31Issue(2)：91-98,8.DOI:10.12132/ISSN.1673-5048.2024.0057
面向可打击区域的高超声速飞行器制导控制一体化方法研究
Research on Integrated Guidance and Control Method for Hypersonic Vehicles for Striking Area
摘要
Abstract
Aiming at the shortcomings of the separation design of guidance and control systems,a method of improving the striking area through integrated design of guidance and control is proposed.Firstly,based on the establishment of an integrated guidance and control model for hypersonic vehicle,the working principle which tracks acceleration commands by controlling the implicated acceleration between the body coordinate sys-tem and the ground coordinate system is revealed.Secondly,through numerical simulation of typical trajecto-ries,the ability of integrated guidance and control design to reduce required overload compared to separate de-sign is compared and analyzed.Finally,by determining the separation and integration design of guidance and control in the striking area of hypersonic vehicle,the advantages of integrated guidance and control are reflected from the perspective of large-scale simulation.The results indicate that the integrated guidance and control can relax the demand for available overload and improve the striking area of hypersonic vehicle.关键词
制导控制一体化/大样本仿真/可打击区域/高超声速飞行器/过载约束Key words
integrated guidance and control/large-scale simulations/striking area/hypersonic vehicles/overload constraint分类
军事科技引用本文复制引用
赵良玉,时皓铭,王建华,崔磊..面向可打击区域的高超声速飞行器制导控制一体化方法研究[J].航空兵器,2024,31(2):91-98,8.基金项目
国家自然科学基金项目(12072027) （12072027）
河南省通用航空技术重点实验室开放基金项目(ZH-KF-230201) （ZH-KF-230201）
