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北京航空航天大学 [31]
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厦门大学 [4]
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Computational study of lateral jet interaction in hypersonic thermochemical non-equilibrium flows using nonlinear coupled constitutive relations
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 11, 页码: 14
作者:
Zeng, Shuhua
;
Yang, Junyuan
;
Zhao, Wenwen
;
Huang YF(黄依峰)
;
Jiang, Zhongzheng
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浏览/下载:0/0
  |  
提交时间:2024/01/22
Appointed-Time Control for Flexible Hypersonic Vehicles with Conditional Disturbance Negation
期刊论文
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2023, 卷号: 59, 期号: 5, 页码: 6327-6345
作者:
Sun, Jinlin
;
Pu, Zhiqiang
;
Chang, Yafei
;
Ding, Shihong
;
Yi, Jianqiang
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浏览/下载:0/0
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提交时间:2024/02/22
Vehicle dynamics
Convergence
Control systems
Aerodynamics
Closed loop systems
Actuators
Mathematical models
Appointed-time control
conditional disturbance negation
hypersonic vehicle
input saturation
prescribed performance control
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System
期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
作者:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
收藏
  |  
浏览/下载:13/0
  |  
提交时间:2022/11/14
Two-stage to orbit
Numerical simulation
Stage separation
Hypersonic flow
Aerodynamic interference
Robust Adaptive Tracking Control for Hypersonic Vehicle Based on Interval Type-2 Fuzzy Logic System and Small-Gain Approach
期刊论文
IEEE TRANSACTIONS ON CYBERNETICS, 2021, 卷号: 51, 期号: 5, 页码: 2504-2517
作者:
Tao, Xinlong
;
Yi, Jianqiang
;
Pu, Zhiqiang
;
Xiong, Tianyi
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  |  
浏览/下载:48/0
  |  
提交时间:2021/06/07
Adaptation models
Aerodynamics
Adaptive systems
Fuzzy logic
Atmospheric modeling
Control design
Vehicle dynamics
Adaptive control
hypersonic vehicle
interval type-2 fuzzy logic system (IT2-FLS)
robust control
small-gain approach
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
作者:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
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  |  
浏览/下载:22/0
  |  
提交时间:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach
期刊论文
IEEE TRANSACTIONS ON NEURAL NETWORKS AND LEARNING SYSTEMS, 2020, 卷号: 31, 期号: 11, 页码: 5005-5013
作者:
Chai, Runqi
;
Tsourdos, Antonios
;
Savvaris, Al
;
Chai, Senchun
;
Xia, Yuanqing
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  |  
浏览/下载:15/0
  |  
提交时间:2021/01/06
Attitude control
Real-time systems
Trajectory optimization
Trajectory planning
Attitude control
bilevel structure
deep neural network (DNN)
six-degree-of-freedom (6-DOF) hypersonic vehicle (HV)
trajectory planning
Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition
期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362
作者:
Wang RX(王睿星)
;
Wang, ZW
;
Zheng HW(郑洪伟)
;
Song HW(宋宏伟)
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  |  
浏览/下载:63/0
  |  
提交时间:2020/06/22
Coupled flow-thermal analysis
Thermal protection system
Basic direct correction method (BDCM)
Improved DCM (IDCM)
Iteration solution method (ISM)
Coupling Model and Electronic Compensation of Antenna-Radome System for Hypersonic Vehicle With Effect of High-Temperature Ablation
期刊论文
IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION, 2020, 卷号: 68, 期号: 3, 页码: 2340-2355
作者:
Wang, Congsi
;
Wang, Yan
;
Chen, Yuankui
;
Gao, Wei
;
Xu, Qian
收藏
  |  
浏览/下载:28/0
  |  
提交时间:2020/06/28
Active phased array antenna
electronic compensation
high-temperature ablation
hypersonic vehicle
performance coupling
A Fast Mathematical Modeling Method for Aerodynamic-Heating Predictions
会议论文
Nagoya, Japan, 2017-07-9~14
作者:
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
收藏
  |  
浏览/下载:30/0
  |  
提交时间:2020/01/06
Conditional disturbance negation based active disturbance rejection control for hypersonic vehicles
期刊论文
CONTROL ENGINEERING PRACTICE, 2019, 卷号: 84, 页码: 159-171
作者:
Sun, Jinlin
;
Pu, Zhiqiang
;
Yi, Jianqiang
收藏
  |  
浏览/下载:58/0
  |  
提交时间:2019/07/12
Active disturbance rejection control
Conditional disturbance negation
Disturbance characterization indicator
Hypersonic vehicle
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