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心的問題之一，是傳熱及其對飛機結構與性能的影響問題。
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，通過高超聲速飛行條件下的仿真，驗證了該方法的有效性。
