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(yǔ)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(jiǎn)單有效的基于規(guī)則的智能阻尼過(guò)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(guó)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(cè)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