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约束条件下的末制导律研究进展
引用本文:张友安,黄诘,王丽英.约束条件下的末制导律研究进展[J].海军航空工程学院学报,2013,28(6):581-586.
作者姓名:张友安  黄诘  王丽英
作者单位:[1]海军航空工程学院控制工程系,山东烟台264001 [2]海军航空工程学院基础部,山东烟台264001
基金项目:基金项目:国家自然科学基金资助项目(61273058)
摘    要:随着武器作战样式的变革,带约束条件下的末制导律研究受到了越来越广泛的关注。评述了近年来约束条件下的末制导律的研究新进展,对目前约束条件下的末制导律设计进行了详细的研究,分析了各种方法的优缺点。在此基础上,对比给出了多约束条件下的末制导律设计的难题以及可能解决的途径。

关 键 词:末制导律  多约束条件  滑模控制  最优控制

Research Progress of Terminal Guidance Law with Constraint
ZHANG You-an,HUANG Jie and WANG Li-ying.Research Progress of Terminal Guidance Law with Constraint[J].Journal of Naval Aeronautical Engineering Institute,2013,28(6):581-586.
Authors:ZHANG You-an  HUANG Jie and WANG Li-ying
Institution:(Naval Aeronautical and Astronautical University a. Department of Control Engineering; b. Department of Basic Sciences, Yantai Shandong 264001, China)
Abstract:With the transformation of weaponry engagement manners, the study of terminal guidance law with constraint condition has drawn extensive attention recently. In this paper, the new progress of the terminal guidance law with con- straint condition in recent years was concentrated, the design of terminal guidance law was studied in detail, the strong- point and defect of all methods was analyzed. Finally, the main difficulties of the terminal guidance law devise for multi- constraints conditions and possible solutions of such difficulties were outlined, which were provided references for re- search on terminal guidance law devise of multi-constraints conditions.
Keywords:terminal guidance law  multi-constraints conditions  sliding-mode control  optimal control
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