终端角度约束制导及制导控制一体化方法综述  

Review of Guidance and Integrated Guidance and Control Methods under Terminal Angle Constraints

作　　者：赵斌[1] 梁乐成 蒋瑞民[1] 周军[1] ZHAO Bin;LIANG Lecheng;JIANG Ruimin;ZHOU Jun(Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]西北工业大学精确制导与控制研究所,西安710072

出　　处：《宇航学报》2022年第5期563-579,共17页Journal of Astronautics

基　　金：国家自然科学基金(61703339);上海航天科技创新基金(SAST2019-004,SAST2020-003,SAST2020-008)。

摘　　要：针对制导武器终端角度约束下的制导方法和制导控制一体化方法进行综述。首先,对比分析了几种典型的终端角度约束定义,针对二维、三维交战场景构建了面向终端角度约束的制导及制导控制一体化设计的状态空间模型;其次,针对终端角度约束下的制导方法以及制导控制一体化设计方法进行分类、归纳总结与对比;最后,针对终端角度约束制导和制导控制一体化设计中存在的多约束落角控制、信息估计、落角范围估计、协同制导等问题进行了展望。Guidance methods and integrated guidance and control(IGC)methods under terminal angle constraints of guided weapons are reviewed.Firstly,several typical definitions of terminal angle constraints are compared and analyzed,and the state space models of the guidance law and IGC method design oriented to terminal angle constraints are constructed for two-and three-dimensional engagement scenarios.Subsequently,the current approaches involving guidance and IGC methods under terminal angle constraints are classified,concluded and compared in detail.Thirdly,the problems of multi-constraint impact angle control,guidance information extraction,impact angle range estimation and cooperative guidance in the guidance and IGC methods under terminal angle constraints are prospected.

关 键 词：终端角度约束 制导律 制导控制一体化 精确制导 

分 类 号：V448.13[航空宇航科学与技术—飞行器设计]