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Nonlinear Control of a Single Tail Tilt Servomotor Tri-Rotor Ducted VTOL-UAV 期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 6, 页码: 17
Authors:  Hu YP(胡延鹏);  Guo, Jin;  Ying, Pei;  Zeng, Guannan;  Chen NY(陈南宇)
Adobe PDF(1020Kb)  |  Favorite  |  View/Download：147/35  |  Submit date：2022/08/10
tail rotor tilting three ducted fan VTOL-UAV  sliding mode NDI  MPC  E-SSPC  super-twisting  disturbance observer  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download：357/178  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
Authors:  Luo ZT(罗长童);  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Li JP(李进平);  Jiang ZL(姜宗林)
View  |  Adobe PDF(2227Kb)  |  Favorite  |  View/Download：289/69  |  Submit date：2019/10/21
Aerodynamic force measurement  Dynamic system  Impact response  Cross-validation  System identification  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
View  |  Adobe PDF(764Kb)  |  Favorite  |  View/Download：360/100  |  Submit date：2017/09/19
Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(764Kb)  |  Favorite  |  View/Download：380/108  |  Submit date：2016/06/28