位置：成果数据库 > 会议 > 会议详情页
Prognostic Management Verification System of Aircraft Hydraulic Power Supply System
  • 所属机构名称：北京航空航天大学
  • 会议名称：Proceedings of IEEE 10th International Conference on Industrial Informatics
  • 时间：2012.7.26
  • 成果类型：会议
  • 相关项目：民用飞机液压泵加速寿命试验基础理论与统计方法研究
作者： 王少萍|韩磊|赵四军|郭春曦|
同会议论文项目
民用飞机液压泵加速寿命试验基础理论与统计方法研究
期刊论文 34 会议论文 34 专利 3 著作 2
同项目会议论文
Design and experimental test of an on-line particle detection sensor based on symmetrical magnetic f
Thermal modeling of axial piston pump and application
A position synchronization control for HA/EHA system
Experimental Analysis of Performance Degradation of Solid Lubricated Bearings with Vibration and Fri
Prognostic management verification system of aircraft hydraulic power supply system
State recognition based on wavelet packet norm entropy for aircraft hydraulic pump
Bearing Fault Diagnosis with an Improved High Frequency Resonance Technique
Integrated reliability theory and evaluation methodology ofAFDX
Overview of Storage Reliability for High Reliability Products
Adaptive Fuzzy Robust Control of a Class of Nonlinear Systems via Small Gain Theorem
Research on the velocity shock and energy loss of T-junction and Arc-juncton in aircraft hydraulic s
Abrasion of on-ff valve side for fuel system
Fluid-solid analysis based on improved bond graph method
Top-level design and all-operation-profile fault reconfiguration strategy for aeroplane hydraulic sy
Top-Level Design and All-Operation-Profile Fault Reconfiguration Strategy for Aeroplane Hydraulic Sy
Fault Simulation Analysis of Axial Piston Pump Based on the Component's Failure
Synchronization Motion Control for Quad-cylinder Lift Systems with Acceleration Coupling
Passive fault-tolerant control for dissimilar redundant actuation system-based on LMI approach
Torsional vibration analysis of a high-speed internal turbine-gearbox using a transfer matrix method
Fault severity recognition of hydraulic piston pumps based on EMD and feature energy entropy
Synchronous controller design for dissimilar redundant actuation system of large civil aircraft
Life Estimation Method of Low-power Sampling System
Modeling of center of gravity of aircraft on multifaults for fuel transfer
Radial Maximum Thermal Network Based on Hollow Cylinder Structure Geometry
Prognostic Analysis Based on Hybrid Prediction Method for Axial Piston Pump
Reliability of Wireless Sensor Network: Hotspot and Critical Challenges
study on change of aircraft center of gravity during fuel consumption
Reliability assessment of aircraft power and actuation system based on three-axis control
Reliability modeling analysis for hydraulic/electro-hydrostatic dual redundant actuation system
An Electronic Pod and its Finite Element Analysis
A Method for Rolling Bearing Fault Diagnosis Based on the Power Spectrum Analysis and Support Vector
Optimization design of Electric servo based on Dynamic performance and Reliability
Reliability growth test based on mission reliability for hydraulic actuation system