海军航空工程学院学报Issue(6)：581-586,6.DOI:10.7682/j.issn.1673-1522.2013.06.001
约束条件下的末制导律研究进展
Research Progress of Terminal Guidance Law with Constraint
摘要
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.关键词
末制导律/多约束条件/滑模控制/最优控制Key words
terminal guidance law/multi-constraints conditions/sliding-mode control/optimal control分类
军事科技引用本文复制引用
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,(6):581-586,6.基金项目
国家自然科学基金资助项目 （）
