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北京航空航天大学 [5]
长春光学精密机械与物... [1]
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会议论文 [3]
期刊论文 [3]
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2018 [3]
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2005 [1]
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Hydraulic piston pump in civil aircraft: Current status, future directions and critical technologies
期刊论文
Chinese Journal of Aeronautics, 2019
作者:
GUO, S.
;
CHEN, J.
;
LU, Y.
;
WANG, Y.
;
DONG, H.
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2019/12/30
Aircraft
Intelligent control
Noise abatement
Pistons
Reciprocating pumps
Seals
Civil aircrafts
Critical technologies
Health management
High pressure
Hydraulic pistons
Inlet boost
Lubricating gaps
Variable displacement
Aircraft hydraulic systems
Simulation of water spray generated by pneumatic aircraft tire on flooded runway
会议论文
AIAA Aerospace Sciences Meeting, 2018, 2018-01-08
作者:
Qu, Q.
;
Liu, T.
;
Liu, P.
;
Agarwal, R.K.
收藏
  |  
浏览/下载:12/0
  |  
提交时间:2019/12/30
Aviation
Constrained optimization
Hydrodynamics
Numerical methods
Tires
Aircraft tires
Civil aircrafts
Coupling interfaces
Numerical calculation
Penalty methods
Smoothed particle hydrodynamics methods
Water sprays
Finite element method
Simulation of Water Spray Generated by Pneumatic Aircraft Tire on Flooded Runway
期刊论文
JOURNAL OF AIRCRAFT, 2018, 卷号: 55, 页码: 1700-1708
作者:
Qu, Qiulin
;
Liu, Ting
;
Liu, Peiqing
;
Agarwal, Ramesh K.
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  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Aircraft
Constrained optimization
Hydrodynamics
Numerical methods
Aircraft tires
Civil aircrafts
Coupling interfaces
Numerical calculation
Penalty methods
Smoothed particle hydrodynamics methods
Water sprays
Tires
Simulation and Evaluation of Civil Aircraft Auto-Landing with Various Guidance Systems
会议论文
Proceedings of 2018 9th International Conference on Mechanical and Aerospace Engineering, ICMAE 2018
作者:
Li, C.
;
Hong, G.
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  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Air navigation
Aircraft
Aircraft landing
Error statistics
Flight control systems
Global positioning system
Radar
Radar systems
Remote control
Auto-landing
Civil aircrafts
Guidance strategy
Guidance system
Performance indices
Preliminary design
Signal statistics
Visual guidance
Aircraft landing systems
Numerical Simulation of Aircraft Tire-Generated Spray and Engine Ingestion on Flooded Runways
期刊论文
JOURNAL OF AIRCRAFT, 2017, 卷号: 54, 页码: 1840-1848
作者:
Zhao, Kaibin
;
Liu, Peiqing
;
Qu, Qiulin
;
Lin, Li
;
Lv, Jun
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  |  
浏览/下载:7/0
  |  
提交时间:2019/12/30
Drops
Engines
Fluid dynamics
Forecasting
Numerical models
Tires
Civil aircrafts
Discrete phase model
Initial conditions
Integrated simulations
Physical interactions
Smoothed particle hydrodynamics
Smoothed particle hydrodynamics methods
Strongly nonlinear
Hydrodynamics
INS's error compensation on the base of the celestial theodolite (EI CONFERENCE)
会议论文
ICO20: Optical Devices and Instruments, August 21, 2005 - August 26, 2005, Changchun, China
Zhao H.-B.
;
Guo L.-H.
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浏览/下载:59/0
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提交时间:2013/03/25
In recent years there has been a major upsurge of interest in the integrated inertial navigation system (INS)/celestial navigation system (CNS) as a cost-effective way of providing accurate and reliable navigation aid for civil and military vehicles (ships
aircrafts
land vehicles and so on). One of the disadvantages of INS is its errors will grow unbounded. The CNS can be used to improve position estimation resulting from INS measurement. This paper describes the design of this. An error model developed earlier is used for CNS/INS filter (Kalman filter) mechanization. In CNS
celestial theodolite acquires an image of the sky
recognize the most brilliant stars in the image
creates with them a "constellation"
and searches for this pattern in an on board star catalogue of the observed region to get the precise position and attitude information of vehicles. The Kalman filter method is used to fuse measurement from the system. We can use this information to compensate INS's error. The tests carry out with this system show that system will get accurate navigation information.
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