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北京航空航天大学 [22]
力学研究所 [7]
西安交通大学 [4]
自动化研究所 [3]
清华大学 [2]
厦门大学 [1]
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期刊论文 [23]
会议论文 [16]
学位论文 [2]
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2020 [1]
2019 [2]
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2017 [5]
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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
收藏
  |  
浏览/下载:17/0
  |  
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
Spectral measurements of hypervelocity flow in an expansion tunnel
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
作者:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Liu YF(刘云峰)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
收藏
  |  
浏览/下载:76/0
  |  
提交时间:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel
Discussion on correlation between wind tunnel test and flight of Mars reentry vehicle [火星再入飞行器风洞试验与真实飞行之间相关性的探讨]
期刊论文
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2019, 卷号: 45, 页码: 787-795
作者:
Liu, F.
;
Yuan, J.
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2019/12/30
Aerodynamics
Correlation methods
Enthalpy
Extrapolation
Heat transfer
Hypersonic aerodynamics
Hypersonic vehicles
Numerical methods
Reentry
Testing
Wind stress
Aerodynamic forces
Aerothermodynamics
Correlation parameters
Extrapolation methods
Flight environment
Mars
Performance parameters
Pressure coefficients
Wind tunnels
钝头体再入气固热耦合计算方法研究
学位论文
北京: 中国科学院大学, 2018
作者:
田保未
收藏
  |  
浏览/下载:67/0
  |  
提交时间:2018/05/31
耦合计算
碳基复合材料
烧蚀
网格移动
重映
Multivariable uniform finite-time output feedback reentry attitude control for RLV with mismatched disturbance
期刊论文
JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2018, 卷号: 355, 页码: 3470-3487
作者:
Tian, Bailing
;
Lu, Hanchen
;
Zuo, Zongyu
;
Zong, Qun
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Attitude control
Closed loop systems
Controllers
Reusability
Robust control
External disturbances
Finite time observers
Finite time stability
Finite-time controllers
Mismatched disturbance
Output feedback controls
Re-usable launch vehicles (RLV)
Robust sliding mode
Feedback
A hybrid numerical scheme for aeroheating computation of hypersonic reentry vehicles
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2018, 卷号: 116, 页码: 432-444
作者:
Gao, Zhen-Xun
;
Xue, Hai-Chao
;
Zhang, Zhi-Chao
;
Liu, Hong-Peng
;
Lee, Chun-Hian
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Aeroheating
Numerical scheme
Hypersonic
Blunt body
Deorbit planning of reentry vehicles using ground track manipulation [基于星下点机动的再入飞行器离轨规划]
期刊论文
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2018, 卷号: 44, 页码: 2141-2148
作者:
Shi, S.
;
Shi, P.
;
Zhao, Y.
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Nonlinear programming
Orbits
Vehicles
Deorbits
Finite thrust
Ground-track
Manipulation methods
Planning method
Re-entry vehicles
Real-time orbits
Trajectory designs
Reentry
Multi-constrained predictor-corrector reentry guidance for hypersonic vehicles
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 卷号: 232, 页码: 3049-3067
作者:
Cheng, Lin
;
Wang, Zhenbo
;
Cheng, Yang
;
Zhang, Qingzhen
;
Ni, Kin
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2019/12/30
Reentry guidance
multi-constrained predictor-corrector algorithm
model identification
period-crossing correction method
constraint management
predictive lateral guidance
Adaptive control of hypersonic vehicles based on characteristic models with fuzzy neural network estimators
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 68, 页码: 475-485
作者:
Chang, Yafei
;
Jiang, Tiantian
;
Pu, Zhiqiang
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2018/03/03
Hypersonic Vehicle
Uncertainty
Time-variation
Characteristic Model-based Adaptive Control
Fuzzy Neural Network Estimator
Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry
会议论文
Xiamen, China, 6-9 March 2017
作者:
Li WH(李文皓)
;
Xiao XX(肖歆昕)
;
Zhang H(张珩)
;
Xiao XX(肖歆昕)
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2018/01/16
Aerodynamics
Air Navigation
Angle Of Attack
Control Surfaces
Control Theory
Degrees Of Freedom (Mechanics)
Dynamic Models
Flight Control Systems
Flight Simulators
Monte Carlo Methods
Reentry
Spacecraft
Surface Reactions
Uncertainty Analysis
Vehicles
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