CAJ | 학술논문

随着导弹等制导武器机动能力的增强,制导精度的提高,多约束条件下的制导律研究成为精确制导研究的新热点.简要介绍了多约束条件下的制导问题,重点评述了近年来多约束条件下的制导律研究情况,对目前多约束条件下的制导律设计进行了比较详细的研究,系统分析了各种方法的优缺点,并分析了其可能的研究内容动态和方向,为精确制导技术的发展提供了参考和借鉴.
수착도탄등제도무기궤동능력적증강,제도정도적제고,다약속조건하적제도률연구성위정학제도연구적신열점.간요개소료다약속조건하적제도문제,중점평술료근년래다약속조건하적제도률연구정황,대목전다약속조건하적제도률설계진행료비교상세적연구,계통분석료각충방법적우결점,병분석료기가능적연구내용동태화방향,위정학제도기술적발전제공료삼고화차감.
With the tide of improving in flexibility and precision of the air-to-surface missile, the study on guidance laws is cared by researchers in precision guidance. After the guidance with impact angular constraints is presented simply, this paper concentrates on the study of the guidance law with impact angular constraints in recent years. In the paper, various guidance laws with impact angular constraints are introduced in detail. We don't only class the articles of guidance law according to the way of design, but also comment on them. Through the trends and direction of the guidance with impact angular constraints are analyzed, the paper can refer the study of the technology of precision guidance.