The orientation theory of the side window was studied and the attitude control law was designed using switch curve method.

以在大氣層高空作戰(zhàn)的動(dòng)能攔截器為物理背景,研究了其側(cè)窗定向的基本原理,采用相平面開關(guān)曲線設(shè)計(jì)了姿態(tài)控制規(guī)律,并進(jìn)行了攔截過程的六自由度數(shù)字仿真。

Control and guide method for side window detection is studied,attitude control law of interceptor is given,and simulation test is done.

由于對(duì)付TBM的高層反導(dǎo)防空導(dǎo)彈速度很高,氣動(dòng)加熱問題十分嚴(yán)重,采用側(cè)窗探測(cè)方式解決氣動(dòng)熱影響問題。

The engagement result is gravely influenced by the side window orientation which involves many factors.

大氣層高層作戰(zhàn)的動(dòng)能攔截器多采用側(cè)窗探測(cè)的結(jié)構(gòu)布局,側(cè)窗定向方位對(duì)其攔截效果有重要的影響,但定向方位的選擇卻受諸多因素制約。