Results 91 to 100 of about 534 (128)

Mathematical modeling and fault detection and diagnosis of an electrohydrostatic actuator [PDF]

open access: yes
This paper studies the mathematical modeling of an electrohydrostatic actuator (EHA) for the purpose of fault detection and diagnosis. A relatively new model-based fault detection strategy referred to as the interacting multiple model and smooth variable
Gadsden SA, Habibi SR, Song Y
core   +1 more source

Performance of an Electro-Hydrostatic Actuator on the F-18 Systems Research Aircraft [PDF]

open access: yes
An electro-hydrostatic actuator was evaluated at NASA Dryden Flight Research Center, Edwards, California. The primary goal of testing this actuator system was the flight demonstration of power-by-wire technology on a primary flight control surface.
Navarro, Robert
core   +1 more source

CONDOR: Long endurance high altitude vehicle, volume 5 [PDF]

open access: yes
The results of a design study resulting in the proposed CONDOR aircraft are presented. The basic requirements are for the aircraft to maintain continuous altitude at or above 45,000 feet for at least a 3-day mission, be able to comfortably support a two ...
Andrews, L. Cullen   +6 more
core   +1 more source

Robust fault diagnosis of an electro-hydrostatic actuator using the novel dynamic second-order SVSF and IMM strategy [PDF]

open access: yes
This paper introduces a new robust fault detection and identification (FDI) structure applied to an electro-hydrostatic actuator (EHA) experimental setup.
Afshari HH, Gadsden SA, Habibi SR
core   +1 more source

A comparison of sigma-point Kalman filters on an aerospace actuator [PDF]

open access: yes
This paper contains a comparison of several sigma-point Kalman filters, including the unscented Kalman filter (UKF), the cubature Kalman filter (CKF), and the central difference Kalman filter (CDKF).
Al-Shabi M   +3 more
core   +1 more source

Analysis, Development and Evaluation of Electro-Hydrostatic Technology for Lower Limb Prostheses Applications* [PDF]

open access: yes, 2020
Amati, Nicola   +5 more
core   +1 more source

More Electric Landing Gear Actuation Study [PDF]

open access: yes, 2009
This report addresses the problem of landing gear actuation system design on more-electric aircraft (MEA). Firstly, information about more-electric aircraft and more-electric actuators was gathered and sorted.
Li, Wei
core  

System Modelling and Bulk Modulus Estimation of an Electrohydrostatic Actuator [PDF]

open access: yes
An electrohydrostatic actuator (EHA) is an emerging type of actuator typically used in the aerospace industry. EHAs are self-contained units comprised of their own pump, hydraulic circuit, and actuating cylinder.
El Delbari SA   +3 more
core  

A Hybrid Swing-Assistive Electro-Hydrostatic Bionic Knee Design [PDF]

open access: yes, 2022
Andrea Tonoli   +6 more
core   +2 more sources

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