Secondly , the method of feedback linearization is adopted to design the automatic landing system 即在保證控制精度的同時(shí),提高閉環(huán)系統(tǒng)的魯棒性。
Firstly , the method of feedback linearization is adopted to design the automatic landing system 論文將非線性系統(tǒng)反饋精確線性化方法應(yīng)用在飛機(jī)自動(dòng)著陸系統(tǒng)的設(shè)計(jì)上。
Automatic landing system of airplane using adaptive inverse control . traffic accidents occur during landing frequently 自適應(yīng)逆控制方法在飛機(jī)自動(dòng)著陸系統(tǒng)中的應(yīng)用。
Adaptive inverse control is applied in the design of automatic landing system and robustness is verified . good simulation results are obtained . at last , nnai is contrasted with the system adopting fuzzy control after linearization 本文以某國(guó)產(chǎn)飛機(jī)為對(duì)象,采用自適應(yīng)逆控制的方法,設(shè)計(jì)飛機(jī)縱向自動(dòng)著陸控制系統(tǒng)并仿真,還對(duì)所設(shè)計(jì)的系統(tǒng)進(jìn)行了魯棒性驗(yàn)證仿真。