A Design Method in Robust Dynamic Boundary Protection System under Condition of Ice Formation on Aircraft by Differential Manifold TheoryLI Yinghui, GUI Yewei, ZUO Renwei, DONG Zehong, ZHANG Jiuxing1-8
Research on the Airflow Separation Structure and Aerodynamic Characteristics of Large Aircraft under Condition of Ice Formation on WingsWEI Yang, LI Jie, LI Ming, LI Zhe, ZHANG Heng9-16,22
Research on Quantitative Evaluation Method of Flight Risk under Condition of Ice Formation on Wings Based on Copula ModelDUAN Xiaocong, XU Haojun, ZHANG Jiuxing, YI Xi'an, XUAN Yuanbo17-22
A Stability Analysis Method for Aircraft's Lateral-Directional System under Condition of Asymmetric Ice Formation on WingsGUO Linliang, WANG Guozhi, PEI Binbin, ZHU Minghong, DAI Shengji23-28
A Fault Diagnosis of SRM Power Converter Based on Current SlopeWANG Rongji, LIU Yongzhi, GUAN Zhenshui29-35
An Adaptive Multistage Observer in Detecting and Isolating Fault in Hydraulic Servo SystemSHEN Xingang, LYU Zhenbang, SUN Qian36-42
A Study of the Influence of Tail Deflection on Landing Skid Performance of AircraftSU Guangxu, ZHANG Dengcheng, WEI Jinpeng, LI Haiquan43-48
Survey on Mixed Reality Military Equipment Maintenance SystemWANG Wei, LEI Songgui, LIU Haiping, LI Taojin, QU Jue, QIU Ang49-54,61
Prediction of Aeroengine Exhaust Gas Temperature Based on Autoencoder-TCN ModelKONG Chenyi, LI Xueren, DU Jun55-61
Air Combat Threat Assessment Based on Prospect Theory and VIKOR MethodHU Tao, WANG Dong, HUANG Zhenyu, SUN Yao, JIANG Longting62-68