Further simplification of the control design process could be realized by dividing the rotorcraft dynamics into translational dynamics and attitude dynamics by using singular perturbation theory.
英
美
- 為了簡(jiǎn)化控制器設計，利用奇異擾動(dòng)理論，把復雜的動(dòng)力學(xué)模型降階為兩個(gè)子系統，即平移動(dòng)力學(xué)和姿態(tài)動(dòng)力學(xué)；
