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Prediction of whirl flutter boundary for tiltrotor aircraft based on BPNN with adaptive data
Lixiong ZHENG, Zhe CHEN, Xin WANG, Qijun ZHAO
doi: 10.7527/S1000-6893.2025.32159
2025, (S1): 732159-732159.
PDF [ 2467 K ]( 361 ) HTML
High-efficiency and high-precision aeroelastic full coupling method of rotor
Xin WANG, Xiayang ZHANG, Lixiong ZHENG, Jinwu XIANG
doi: 10.7527/S1000-6893.2025.32161
2025, (S1): 732161-732161.
PDF [ 3956 K ]( 477 ) HTML
Aerodynamic interference of scissor tail rotor and influence of unconventional layout parameters
Wangqing ZHU, Chenkai CAO, Guoqing ZHAO, Qinghua ZHU, Haoyu HU
doi: 10.7527/S1000-6893.2025.32181
2025, (S1): 732181-732181.
PDF [ 4306 K ]( 205 ) HTML
Optimization design of high-efficiency and low-noise rotor layout for quad-tiltrotor aircraft
Xiayang ZHANG, Bin LUO, Xi CHEN, Tao YANG
doi: 10.7527/S1000-6893.2025.32183
2025, (S1): 732183-732183.
PDF [ 6861 K ]( 430 ) HTML
Design of reward functions for helicopter attitude control in reinforcement learning
Tao ZHANG, Pan LI, Zixu WANG, Zhenhua ZHU
doi: 10.7527/S1000-6893.2025.32184
2025, (S1): 732184-732184.
PDF [ 3701 K ]( 563 ) HTML
Brownout suppression optimization of helicopter landing trajectory parameters under real control
Zhuangzhuang CUI, Binwu REN, Xu ZHOU, Zhe CHEN, Guoqing ZHAO
doi: 10.7527/S1000-6893.2025.32186
2025, (S1): 732186-732186.
PDF [ 4842 K ]( 181 ) HTML
Direct numerical simulation of supersonic turbulent boundary layer with plasma actuation
Chen LI, Dong SUN, Pengxin LIU, Qilong GUO, Xianxu YUAN
doi: 10.7527/S1000-6893.2025.32187
2025, (S1): 732187-732187.
PDF [ 3411 K ]( 214 ) HTML
Adaptive attitude control for tilt-quadrotor UAV based on ADRC-RBF
Jiong HE, Binwu REN, Siliang DU, Yousong XU, Bo WANG
doi: 10.7527/S1000-6893.2025.32189
2025, (S1): 732189-732189.
PDF [ 3767 K ]( 597 ) HTML
Autonomous decision-making in close-range game under imperfect information for unmanned aerial vehicles
Pan ZHOU, Ni LI, Jiangtao HUANG, Qinglin YANG, Yunxiao LIAN
doi: 10.7527/S1000-6893.2025.32215
2025, (S1): 732215-732215.
PDF [ 3400 K ]( 532 ) HTML
Aerodynamic influence study of ducted tail rotor geometry and configuration parameters
Zhicheng LIU, Feng LIAO, Chenkai CAO, Wangqing ZHU, Guoqing ZHAO, Qijun ZHAO, Haoyu HU
doi: 10.7527/S1000-6893.2025.32224
2025, (S1): 732224-732224.
PDF [ 5301 K ]( 381 ) HTML
Fault diagnosis of spacecraft attitude control system driven by data and model
Ronghai KOU, Wenbo LI, Qingqing DANG, Jinjin XIE
doi: 10.7527/S1000-6893.2025.32259
2025, (S1): 732259-732259.
PDF [ 3192 K ]( 839 ) HTML
Powered yaw predictive control of distributed electric propulsion aircraft considering slipstream effects
Zhihao HE, Peng KOU, Bohua LIANG, Deliang LIANG
doi: 10.7527/S1000-6893.2025.32305
2025, (S1): 732305-732305.
PDF [ 2813 K ]( 396 ) HTML
Effects of adjustable guide vanes coupled with partial admission on turbine aerodynamic performance
Wei JIA, Xiao MA, Lei QI, Weihao ZHANG, Zhihong ZHOU
doi: 10.7527/S1000-6893.2025.32306
2025, (S1): 732306-732306.
PDF [ 7040 K ]( 160 ) HTML
Simulation and experiment of attitude control propulsion system’s dynamic characteristics
Fang ZHANG, Weibin XIANG, Kai XIAO, Siqi XIAO, Liang XIANG, Bing WANG
doi: 10.7527/S1000-6893.2025.32329
2025, (S1): 732329-732329.
PDF [ 3180 K ]( 218 ) HTML
Aerodynamic parameter identification of launch vehicle based on offline learning and online correction
Bichen HU, Liangliang HU, Yuxi LIU, Shujun TAN
doi: 10.7527/S1000-6893.2025.32407
2025, (S1): 732407-732407.
PDF [ 2000 K ]( 213 ) HTML
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