基本解釋[機(jī)械工程]飛航導(dǎo)彈[交通運(yùn)輸工程]有翼導(dǎo)彈[航空、航天科學(xué)技術(shù)]有翼導(dǎo)彈英漢例句雙語例句Then, a simple effective overload control method for winged missile using intelligent resistance is presented.然后給出了一種簡單有效的基于規(guī)則的智能阻尼過載控制方法。winged missile更多例句專業(yè)釋義機(jī)械工程飛航導(dǎo)彈While designing winged missile flight control system, attitude stable scheme is traditional selected in our country. The method means that measuring the missile attitude angles and angle-rate by sensor, attitude angular PID control is executed by close loop.在設(shè)計(jì)飛航導(dǎo)彈的飛行控制系統(tǒng)時(shí)，國內(nèi)一般采用傳統(tǒng)的姿態(tài)穩(wěn)定控制方案，即由敏感元件測量導(dǎo)彈的空間姿態(tài)角和姿態(tài)角速度，形成閉合回路，進(jìn)行姿態(tài)角的PID控制。交通運(yùn)輸工程有翼導(dǎo)彈航空、航天科學(xué)技術(shù)有翼導(dǎo)彈