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长春光学精密机械与物... [2]
北京大学 [1]
西安交通大学 [1]
北京航空航天大学 [1]
福州大学 [1]
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会议论文 [3]
期刊论文 [3]
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2018 [4]
2017 [1]
2011 [1]
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AN ANALYSIS MODEL TO PREDICT ROTATION ACCURACY OF HIGH-PRECISION SPINDLES CONSIDERING PART ERRORS AND DEFORMATION
会议论文
作者:
Sun, Yanhui
;
Hong, Jun
;
Guo, Junkang
;
Zhang, Yanfei
;
Wan, Shaoke
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/11/19
high-precision spindle
rotation accuracy
formation
error accumulation
geometric error
Sensor-Based Inspection of the Formation Accuracy in Ultra-Precision Grinding (UPG) of Aspheric Surface Considering the Chatter Vibration
期刊论文
PHOTONIC SENSORS, 2018, 卷号: 8, 页码: 97-102
作者:
Lei, Yao
;
Bai, Yue
;
Xu, Zhijun
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  |  
浏览/下载:8/0
  |  
提交时间:2019/11/21
micro-vibrations
Optical aspheric surface
grinding speed
formation accuracy
ultra-precision grinding
Adaptive genetic algorithm-based method for antenna location optimization in RF relative measurement
会议论文
2018 NASA/ESA Conference on Adaptive Hardware and Systems, AHS 2018
作者:
Zijie, W.
;
Rongke, L.
;
Weiqing, M.
;
Xiaoyan, S.
;
Thompson, J.
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  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Genetic algorithms
Location
NASA
Spacecraft
Spacecraft propulsion
Adaptive genetic algorithms
Antenna location optimizations
Antenna locations
Function optimization problems
Measurement accuracy
Relative measurement
Relative position and attitude
Spacecraft formation flying
Antennas
Sensor-Based Inspection of the Formation Accuracy in Ultra-Precision Grinding (UPG) of Aspheric Surface Considering the Chatter Vibration
期刊论文
Photonic Sensors, 2018, 卷号: 8, 期号: 2, 页码: 97-102
作者:
Lei, Y.
;
Bai, Y.
;
Xu, Z. J.
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  |  
浏览/下载:4/0
  |  
提交时间:2019/09/17
Optical aspheric surface
micro-vibrations
ultra-precision grinding
formation accuracy
grinding speed
system
Instruments & Instrumentation
Optics
Significantly Improved Protein Folding Thermodynamics Using a Dispersion-Corrected Water Model and a New Residue-Specific Force Field
期刊论文
JOURNAL OF PHYSICAL CHEMISTRY LETTERS, 2017
Wu, Hao-Nan
;
Jiang, Fan
;
Wu, Yun-Dong
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浏览/下载:3/0
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提交时间:2017/12/03
MOLECULAR-DYNAMICS SIMULATIONS
INTRINSICALLY DISORDERED PROTEINS
ALPHA-HELIX FORMATION
SIDE-CHAIN
BACKBONE PARAMETERS
AMBER FF99SB
PEPTIDES
COOPERATIVITY
ACCURACY
EXCHANGE
Adaptive control at launching using three loop autopilot (EI CONFERENCE)
会议论文
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
Zhang Y.
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浏览/下载:18/0
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提交时间:2013/03/25
In order to guarantee the precise initial flight trajectory
control the missile disturbance of large disturbance torque
three loop adaptive autopilot was researched. The characteristics of the projectile and three loop autopilot instruction formation characteristics were analysed. From equivalent pitching angle of lateral acceleration feedback loop
combined with the instruction of generalized error
autopilot structure was simplified
and three loop autopilot adaptive control law and stability were designed. The test data show that when disturbance torque was 600Nm
the attitude angle generalized error was -4.4. In the time lasted about 15s
late trajectory accuracy was within 1.0.Three loop autopilot adaptive control law was able to control the disturbance of initial trajectory and adapt to dynamic characteristics changes
control system stability. It was the initial trajectory accurate solution method of flight. 2011 IEEE.
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