Results 171 to 180 of about 3,270 (221)

Multiscale Modeling of Thermo-Electro-Mechanical Coupling of BGA Solder Joints in Microelectronic Systems of Ruggedized Computers for Signal Integrity Analysis. [PDF]

Micromachines (Basel)
Li P, Huang J, Zhang J, Gong H, Wang J, Zuo D, Su M, Shi J.   +7 more
europepmc   +1 more source

Application-oriented classification and performance analysis of precision linear feed mechanisms for machine tools. [PDF]

Sci Prog
Zhou J, Yu H, He M, Zhang Y, Luan X, Liu Y.   +5 more
europepmc   +1 more source

Fault Diagnosis and Fault Handling for Autonomous Aircraft [PDF]

, 2012
Adrian, Jens, Blanke, Mogens, Hansen, Søren   +2 more
core  

Permeability evolution and microstructural regulation of clay cement grouted body under coupled seepage and stress conditions. [PDF]

Sci Rep
Lujun C, Yaoxiang W, Kun W, Aiping C.
europepmc   +1 more source

Green synthesis of building blocks, drug candidates and fine chemicals by barochemistry: application of high pressure in organic synthesis.

Green Chem
Xie G, Wright V, Lazarev A, Smejkal G, Gross V, Török B.   +5 more
europepmc   +1 more source

Some of the next articles are maybe not open access.

Related searches:

Review on electro hydrostatic actuator for flight control

International Journal of Fluid Power, 2016
AbstractElectro Hydrostatic Actuator (EHA) is an emerging aerospace technology that aims at replacing centralised hydraulic system by a self-contained and localised direct drive actuator system. EHA has become an important part of modern flight control systems due to the increased efficiency, reduced leakages and lower overall weight compared to ...
Somashekhar S Hiremath, Makaram Singaperumal, Apratim Talukdar   +2 more
exaly   +2 more sources

MODELLING AND CONTROL OF AN ELECTRO‐HYDROSTATIC ACTUATOR

International Journal of Robust and Nonlinear Control, 1997
The control of a novel aerospace actuator is considered, viz., an electro-hydrostatic actuator. It offers a high degree of maintainability and combat survivability of the aircraft's flight control system because all the actuator's elements are collocated.
Pachter, M., Houpis, C. H., Kang, K.
openaire   +2 more sources

Electro-Hydrostatic Actuator Modeling

Applied Mechanics and Materials, 2013
This paper demonstrates the modeling of an Electro-Hydrostatic Actuator prototype. The mathematical derivation of the physical model is reported.Parametric model was obtained through system identification.
Yu Song, S.R. Habibi
openaire   +1 more source