Conceptual design and preliminary experiment of icing risk management and protection system  

作　　者：Qiang WU Haojun XU Binbin PEI Yang WEI 

机构地区：[1]School of Aeronautics Engineering,Air Force Engineering University,Xi’an 710038,China

出　　处：《Chinese Journal of Aeronautics》2022年第6期101-115,共15页中国航空学报（英文版）

基　　金：co-supported by the National Basic Research Program of China (No. 2015CB755802);the National Natural Science Foundation of China (No. 61873351 and No. 62103440)

摘　　要：Icing is one of the main external environmental factors that causes aircraft to lose control.The flight safety assurance system under icing condition is particularly important.However,most of the systems do not consider the coupling characteristics of aerodynamics and flight dynamics of icing aircraft.This will affect the accuracy of the calculation results.Besides,the icing risk management system helps the pilot to realize the possible dangers in advance and perform correct maneuvers,based on quantitative assessment and visualization methods of flight risk.The envelope protection system realizes flight safety guarantee based on the real-time boundary protection method of key flight parameters.Finally,based on distributed simulation technology,a flight simulator was used as a platform to integrate the icing risk management system and envelope protection system to realize man-in-the-loop simulation.Two fictional but historically motivated icing scenarios are designed to test the system,and the results demonstrate that the icing risk management and protection system would be useful for aviation safety and can also be used for pilot training and reproducing flight accidents to find the causes.

关 键 词：Flight risk Flight simulator ICING Quantitative assessment VISUALIZATION 

分 类 号：V328[航空宇航科学与技术—人机与环境工程] V244.15