J113014 Prototype Model of Flight Simulator Using Tripod Parallel Mechanism : Evaluation of Motion with Washout Algorithm

2012 ◽  
Vol 2012 (0) ◽  
pp. _J113014-1-_J113014-4
Author(s):  
Shohei ARAI ◽  
Hitomi KONDO ◽  
Hiroyuki GOTO ◽  
Yutaka TANAKA
Keyword(s):  
Parallel Mechanism ◽  
Flight Simulator ◽  
Prototype Model ◽  
Washout Algorithm

scholarly journals J112013 Prototype Model of Flight Simulator Using Tripod Parallel Mechanism

2011 ◽  
Vol 2011 (0) ◽  
pp. _J112013-1-_J112013-4
Author(s):  
Yutaka TANAKA ◽  
Shohei ARAI ◽  
Hitomi KONDO ◽  
Yoshito TANAKA
Keyword(s):  
Parallel Mechanism ◽  
Flight Simulator ◽  
Prototype Model

Prototype model of tripod parallel mechanism with planar actuators for flight simulator

2011 ◽  
Author(s):  
Hitomi Kondo ◽  
Yuichi Shiga ◽  
Yutaka Tanaka ◽  
Hiroyuki Goto
Keyword(s):  
Parallel Mechanism ◽  
Flight Simulator ◽  
Prototype Model

S113024 Design and Evaluation of Tripod Parallel Mechanism for flight Simulator

2011 ◽  
Vol 2011 (0) ◽  
pp. _S113024-1-_S113024-4
Author(s):  
Yutaka TANAKA ◽  
Ryo AIZAWA ◽  
Yuichi SHIGA ◽  
Hiroyuki GOTO
Keyword(s):  
Parallel Mechanism ◽  
Flight Simulator

The Influence of Payload Mass and Inertia Properties on a Piloted Flight Simulator Hexapod Dynamic Performance

2014 ◽  
Vol 1037 ◽  
pp. 61-65
Author(s):  
Chun Ping Pan ◽  
Ying Lu ◽  
Yi Jun Lin
Keyword(s):  
Parallel Mechanism ◽  
High Speed ◽  
Dynamic Performance ◽  
Flight Simulator ◽  
Dynamics Model ◽  
The Real ◽  
High Acceleration ◽  
Inertia Properties ◽  
Payload Mass

In order to improve the dynamic performance of a piloted flight simulator hexapod, a study was carried out to quantify the effects of payload mass and inertia properties on hexapod dynamic performance. Based on the Lagrange-Euler formulation, a dynamics model of hexapod parallel mechanism including the payload mass characteristics was built, and then analyzed with the real hexapod through experiments. According to a large amount of experiment datum, the influence of payload mass and inertia properties on a piloted flight simulator hexapod dynamic performance was obtained, and these results are significant for the high speed and high acceleration control of the hexapod mechanism.

J114033 Motion Analysis of Flight Simulator for Tripod Parallel Mechanism with Planar Actuators

2013 ◽  
Vol 2013 (0) ◽  
pp. _J114033-1-_J114033-5
Author(s):  
Yutaka TANAKA ◽  
Gaku MINORIKAWA ◽  
Hiroshi TAKEDA
Keyword(s):  
Motion Analysis ◽  
Parallel Mechanism ◽  
Flight Simulator

Hydraulic System Simulation of 3-UPS Parallel Mechanism Based on ADAMS/Hydraulics

2013 ◽  
Vol 579-580 ◽  
pp. 430-433
Author(s):  
Bing Bing Yan ◽  
Wen Bo Ren ◽  
Bao Lin Yin ◽  
Yang Li
Keyword(s):  
Hydraulic System ◽  
Parallel Mechanism ◽  
Simulation Analysis ◽  
Theoretical Calculations ◽  
Three Dimensional ◽  
Hydraulic Cylinder ◽  
Prototype Model ◽  
Pressure Curve ◽  
Hydraulic Control ◽  
Coupling System

In order to guaranty the work stability of the move-in-mud robot and movement relationship of wriggle turning joint, to use the 3-UPS parallel mechanism as the steering joint. Make full use of the characteristics flexibility, heavy force loading and small workspace of the parallel mechanism. Supporting link of the parallel mechanism driven by hydraulic cylinders, so a completely hydraulic system is an important factor to ensure the stationary work of parallel mechanism, provide the required power to go forward and ensure the forward speed of the move-in-mud robot. Establish the virtual prototype model of mechanical-hydraulic coupling system by using of Pro/E and ADAMS/Hydraulics software, do the dynamic simulation analysis of hydraulic control system based on Hydraulics module, the simulation process can be made more visual and vivid by three-dimensional visualization. Obtain the platform speed and hydraulic cylinder pressure curve after simulation, compare simulation results with theoretical calculations, and verify that the design is reasonable. The results show that it lays the foundation for the further optimization and research of the move-in-mud robot.

Design of a 6 D.O.F. Flight Simulator Based on a Full Spinning Parallel Mechanism Platform

2005 ◽  
Author(s):  
Sun Ho Kim ◽  
Hyun Pyo Shin ◽  
Woo Sung In ◽  
Jongwon Kim
Keyword(s):  
Parallel Mechanism ◽  
Flight Simulator

An Alternative Method for Identifying a Failed Engine in Twin-Engine Propeller Aircraft

2020 ◽  
Vol 10 (2) ◽  
pp. 103-111
Author(s):  
Andrey K. Babin ◽  
Andrew R. Dattel ◽  
Margaret F. Klemm
Keyword(s):  
Human Error ◽  
Flight Simulator ◽  
Traditional Group ◽  
Aircraft Accidents ◽  
Alternative Method ◽  
Indicator Group ◽  
Group A ◽  
The Dead ◽  
Engine Failure ◽  
And Performance

Abstract. Twin-engine propeller aircraft accidents occur due to mechanical reasons as well as human error, such as misidentifying a failed engine. This paper proposes a visual indicator as an alternative method to the dead leg–dead engine procedure to identify a failed engine. In total, 50 pilots without a multi-engine rating were randomly assigned to a traditional (dead leg–dead engine) or an alternative (visual indicator) group. Participants performed three takeoffs in a flight simulator with a simulated engine failure after rotation. Participants in the alternative group identified the failed engine faster than the traditional group. A visual indicator may improve pilot accuracy and performance during engine-out emergencies and is recommended as a possible alternative for twin-engine propeller aircraft.

Flight simulator runway visual textural cues for landing.

1980 ◽  
Author(s):  
George H. Buckland ◽  
Eric G. Monroe ◽  
Kent I. Mehrer
Keyword(s):  
Flight Simulator
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