One of the most interesting contemporary problems of flight at high supersonic speed is that of heat transfer and its effects on aircraft performance and structure. 當代高超聲速飛行最關(guān)心的問(wèn)題之一，是傳熱及其對飛機結構與性能的影響問(wèn)題。
The proposed method is used to design the flight control system of ASV, and simulation results show that the method has excellent performence and strong robustness. 最后利用該方案設計出空天飛行器飛行控制系統，通過(guò)高超聲速飛行條件下的仿真，驗證了該方法的有效性。
