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终端角度约束制导及制导控制一体化方法综述
引用本文:赵斌,梁乐成,蒋瑞民,周军. 终端角度约束制导及制导控制一体化方法综述[J]. 宇航学报, 2022, 43(5): 563-579. DOI: 10.3873/j.issn.1000-1328.2022.05.003
作者姓名:赵斌  梁乐成  蒋瑞民  周军
作者单位:西北工业大学精确制导与控制研究所,西安 710072
基金项目:国家自然科学基金(61703339);
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。

关 键 词:终端角度约束  制导律  制导控制一体化  精确制导  
收稿时间:2021-07-09

Review of Guidance and Integrated Guidance and Control Methods under Terminal Angle Constraints
ZHAO Bin,LIANG Lecheng,JIANG Ruimin,ZHOU Jun. Review of Guidance and Integrated Guidance and Control Methods under Terminal Angle Constraints[J]. Journal of Astronautics, 2022, 43(5): 563-579. DOI: 10.3873/j.issn.1000-1328.2022.05.003
Authors:ZHAO Bin  LIANG Lecheng  JIANG Ruimin  ZHOU Jun
Affiliation:Institute of Precision Guidance and Control, Northwestern Polytechnical University, Xi’an 710072, China
Abstract: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.
Keywords:Terminal angle constraint  Guidance law  Integrated guidance and control  Precision guidance  
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