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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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先进制造工艺力学实验... [5]
Laboratory... [1]
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张珩 [5]
李文皓 [4]
肖歆昕 [4]
冯冠华 [1]
刘开磊 [1]
郭正雄 [1]
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宇航学报 [2]
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控制理论与应用 [1]
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Indexed By:EI
Creator:张珩
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间隙引发的变载非线性及其闭环辨识
期刊论文
控制理论与应用, 2019, 卷号: 36, 期号: 05, 页码: 673-679
Authors:
张珩
;
肖歆昕
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View/Download:336/56
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Submit date:2019/09/12
间隙变载非线性
间隙闭环辨识
非线性效应
描述函数
自激振荡
Space Robot Teleoperation Experiment and System Evaluation Method
会议论文
2018 2nd IEEE Advanced Information Management,Communicates,Electronic and Automation Control Conference (IMCEC), China, 25-27 May 2018
Authors:
Feng GH(冯冠华)
;
Li WH(李文皓)
;
Zhang H(张珩)
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Submit date:2018/10/29
Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li WH(李文皓)
;
Xiao XX(肖歆昕)
;
Zhang H(张珩)
;
Xiao XX(肖歆昕)
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Submit date: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
地球大气边缘高超声速飞行再入点调整方法
期刊论文
宇航学报, 2013, 卷号: 34, 期号: 7, 页码: 946-954
Authors:
郭正雄
;
张珩
;
肖歆昕
;
李文皓
;
刘开磊
;
马欢
Adobe PDF(1036Kb)
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Submit date:2013/09/02
地球大气边缘
高超声速
再入点调整
神经网络i-pida
模糊预测制导
降低亚轨道飞行器再入法向过载峰值的攻角设计方法
期刊论文
宇航学报, 2012, 卷号: 33, 期号: 1, 页码: 40-47
Authors:
肖歆昕
;
李文皓
;
张珩
Adobe PDF(848Kb)
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View/Download:728/267
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Submit date:2013/01/16
亚轨道
飞行器
再入
攻角设计
法向过载动态平衡