Results 51 to 60 of about 534 (128)

Preliminary design and multi-objective optimization of electro-hydrostatic actuator [PDF]

open access: yes, 2016
Electro-hydrostatic actuator is generally regarded as the preferred solution for more electrical aircraft actuation systems. It is of importance to optimize the weight, efficiency and other key design parameters, during the preliminary design phase. This
Bo Yu   +4 more
core   +1 more source

车辆电动静液压主动悬架系统的设计与试验研究

open access: yesJixie chuandong, 2009
A active suspension system with EHA(Electro-Hydrostatic Actuator) is developed to improve the ride comfort performance using a fuzzy PID control scheme,which makes the control system more intelligent.The performance of the controller can be improved by ...
寇发荣
doaj  

Analysis and Improvement of the Dynamic Characteristics of an Electro-Hydrostatic Actuator Based on a Vehicle’s Active Suspension

open access: yesWorld Electric Vehicle Journal
This study investigates the dynamic characteristics of electro-hydrostatic actuators (EHA), which serve as the core actuating element in vehicle active suspension systems, with the aim of enhancing overall system performance. The purpose of this research
Peng Chen, Xing Chen
doaj   +1 more source

Indirect aircraft control systems [PDF]

open access: yes, 2011
Bakalářská práce se zabývá popisem vybraných prvků v soustavách řízení letadel a jejich začleněním do těchto soustav. Uvedeny jsou rovněž požadavky předpisů na spolehlivost soustav řízení.
Kalný, Jan
core  

A Qualitative and Quantitative Functional Modelling Method for PHM System Design

open access: yesChemical Engineering Transactions, 2013
In the early stage of PHM system design, it is very important to analyse the failure modes and their effects,i.e. FMEA. A great number of model-based methods have been proposed recently; however, the analysis process might concern only qualitative or ...
L. Song   +4 more
doaj   +1 more source

Synthesis of an electro hydrostatic actuator from bicausal bond graphs [PDF]

open access: yes, 2007
In this paper, the structure of an Electro Hydrostatic Actuator (EHA) devoted to flight control surfaces is firstly described by its Causal Bond Graph (CBG).
Gandanegara, Grace   +3 more
core  

Review of Development Stages in the Conceptual Design of an Electro Hydrostatic Actuator for Robotics [PDF]

open access: yes, 2014
The design of modern robotic devices faces numerous requirements and limitations which are related to optimization and robustness. Consequently, these stringent requirements have caused improvements in many engineering areas and lead to development of ...
Jocanović, Mitar   +2 more
core   +1 more source

ASSESSMENT OF NEW TECHNOLOGIES IN A MULTI-DISCIPLINARY DESIGN ANALYSIS AND OPTIMIZATION ENVIRONMENT INCLUDING RAMS AND COST DISCIPLINES [PDF]

open access: yes, 2021
The aim of the present paper is to assess the effect of new technologies on the whole aircraft product including its costs, reliability and maintainability characteristics.
Boggero L.   +5 more
core  

Multi-Objective Optimal Design of Electro-Hydrostatic Actuator Driving Motors for Low Temperature Rise and High Power Weight Ratio

open access: yesEnergies, 2018
With the rapid development of technology, motors have drawn increasing attention in aviation applications, especially in the more electrical aircraft and all electrical aircraft concepts.
Guo Hong   +3 more
doaj   +1 more source

Energy efficient design of regenerative shock absorbers for automotive suspensions: A multi-objective optimization framework [PDF]

open access: yes
This study addresses the optimized design of electro-hydrostatic regenerative shock absorbers to enhance vibrational energy recovery in ground vehicles, aiming to reduce carbon footprint.
Amati, Nicola   +4 more
core   +1 more source

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