Results 51 to 60 of about 534 (128)
Preliminary design and multi-objective optimization of electro-hydrostatic actuator [PDF]
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
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
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]
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
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]
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]
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]
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
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]
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

