导弹/火箭制导、导航与控制技术发展与展望  

Review and Prospect of Missile/Launch Vehicle Guidance, Navigation and Control Technologies

作　　者：马卫华[1,2,3] MA Wei-hua(Beijing Aerospace Automatic Control Institute,Beijing 100854,China;National Key Laboratory of Science and Technology on AerospaceIntelligence Control,Beijing 100854,China;Aerospace Intelligent Technology Innovation Center,Beijing 100854,China)

机构地区：[1]北京航天自动控制研究所,北京100854 [2]宇航智能控制技术国家级重点实验室,北京100854 [3]航天智能技术创新中心,北京100854

出　　处：《宇航学报》2020年第7期860-867,共8页Journal of Astronautics

基　　金：国家自然科学基金(61603365)。

摘　　要：本文对导弹/火箭制导、导航与控制(GNC)技术的发展进行了综述。总结归纳了不同阶段GNC关键技术的突破与跨越,重点对惯性导航、组合导航、摄动制导、闭路制导、迭代制导、频域设计、全数字设计、冗余控制、自适应控制等多项技术进行了总结和应用成果论述。对未来GNC技术的发展进行了思考与展望,并提出了七项关键技术。针对更聪明、更自主的弹/箭控制技术发展需求,提出并分析了"会学习"弹/箭的制导、导航与控制技术。This paper reviews the development and achievements of the guidance,navigation and control(GNC)technologies for missiles/launch vehicles.Some important breakthroughs and leapfrogs of GNC key technologies in different stages are summarized.Then,the article mainly focuses on the summary and applications of the inertial navigation,integrated navigation,perturbation guidance,close-loop guidance,iterative guidance,digital design,redundant control,adaptive control and other technologies.This paper considers and prospects the future development direction of China’s GNC technologies,and puts forward seven key technologies.At last,in order to meet the needs of"more intelligent and more autonomous"of the future missiles/launch vehicles,this paper proposes a new concept of launch vehicle named"Self-learning"missile/launch vehicle,and analyses the features of its GNC technologies.

关 键 词：导弹/火箭 制导、导航与控制(GNC) 

分 类 号：V448.1[航空宇航科学与技术—飞行器设计]