نتایج جستجو برای: propulsion system

تعداد نتایج: 2236696  

Journal: :IOP conference series 2023

Abstract The paper presents the results of development a neutralizer-free high-frequency ion thruster for university nanosatellite propulsion systems which allow it to perform orbit correction tasks. application technologies allows self-neutralization mode and is relevant engines CubeSat format small satellites where size weight system must be as minimal possible. A pair shapes thrusters with d...

Journal: :The International Conference on Applied Mechanics and Mechanical Engineering 2012

Journal: :TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 2016

Journal: :IEEE Aerospace and Electronic Systems Magazine 2001

Journal: :JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2011

2016
Dmitry Bershadsky Stephen Haviland Eric N. Johnson

One of the more daunting tasks of designing a multirotor unmanned aerial vehicle (UAV) is the selection of a propulsion system that will provide desired performance. Rigorous methods for selecting these drive components, that is, the motors, propellers, and batteries for electric UAVs are not readily available. Currently, many UAV designs are based on legacy selections or limited and at times i...

2006
Murat Yasar Asok Ray

This paper presents an application of the recently developed theory of language-measure-based discrete event supervisory (DES) control to aircraft propulsion systems. A two-layer hierarchical architecture is proposed to coordinate the operations of a twin-engine propulsion system. The two engines are individually controlled to achieve enhanced performance and reliability, as necessary for fulfi...

2015
Amirhossein Adami Mahdi Mortazavi Mehran Nosratollahi Chen Gang Xu Min Rajesh Kumar Arora Pradeep Kumar M. Mortazavi A. Adami M. Hosseini Mehdi Mortazavi Majid Hosseini

Unguided reentry capsules are usually involved in ballistic entry. The final states (such as altitude and velocity of parachute activity) depend on initials parameters. Reentry trajectory parameters differently affect the thermal protection system (TPS), required deorbit propellant, and structural load. The purpose of this paper is to optimal design of deorbit parameters to minimize the thermal...

Journal: :American journal of physical medicine & rehabilitation 2002
Rachid Aissaoui Hossein Arabi Michèle Lacoste Vincent Zalzal Jean Dansereau

OBJECTIVE To investigate the effects of the system tilt and back recline angles on the biomechanics of wheelchair propulsion for a group of older, disabled patients. It was hypothesized that increasing both the system tilt and backrest recline angles would have a positive effect on the biomechanical efficiency of manual wheelchair propulsion. DESIGN Three kinetic variables were estimated duri...

2015
U. Campora C. Cravero R. Zaccone

The paper presents the application of artificial neural network for simulation and diagnostic purposes applied to a gas turbine powered marine propulsion plant. A simulation code for the propulsion system, developed by the authors, has been extended to take into account components degradation or malfunctioning with the addition of performance reduction coefficients. The above coefficients becom...

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