CAJ | 학술논문

传递对准是解决机载战术导弹在空中动基座条件下初始对准问题的有效方法.为有效估计机载战术导弹系统的姿态误差角,文中在基本匹配方案的基础上,详细研究了"角速率+比力"匹配和"速度+全姿态矩阵"匹配这两种传递对准的匹配方案,分别推导了其数学模型,并进行了数字仿真,最后对仿真的结果进行了比较、分析,结果表明该方法能够有效的估计姿态误差角,并能够在较短时间内以一定精度完成初始对准.
전체대준시해결궤재전술도탄재공중동기좌조건하초시대준문제적유효방법.위유효고계궤재전술도탄계통적자태오차각,문중재기본필배방안적기출상,상세연구료"각속솔+비력"필배화"속도+전자태구진"필배저량충전체대준적필배방안,분별추도료기수학모형,병진행료수자방진,최후대방진적결과진행료비교、분석,결과표명해방법능구유효적고계자태오차각,병능구재교단시간내이일정정도완성초시대준.
Transfer alignment is the effective method of solving the problem of initial alignment for airborne tactical missile on moving base. Aiming at the airborne tactical missile system, on the basis of basic matching schemes, the"velocity+attitude matrix" matching and the "angular rate+specific force"matching schemes are entirely researched in this thesis, and their mathematic models are derived respectively. Then the simulations of them are made and the analysis of the simulation results is made. The result shows that the algorithm can effectively estimate the misalignment, and realize the transfer alignment with certain accuracy in short time.