Recently higher requirments on the flying quality of the lateral control system of a tailless aircraft make the traditional approach to its parameter-optimal design increasingly less applicable.
英
美
- 詳細研究了無(wú)尾飛機橫側向系統的穩定性,并針對該無(wú)人機橫側向控制系統,運用經(jīng)典的控制方法,通過(guò)優(yōu)化而自動(dòng)調節控制律參數的一種時(shí)域方法設計控制律,優(yōu)化算法采用序列二次規劃方法。
