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

Chun Ping Pan; Ying Lu; Yi Jun Lin

doi:10.4028/www.scientific.net/AMR.1037.61

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 1037The Influence of Payload Mass and Inertia...

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

Abstract:

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.

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Periodical:

Advanced Materials Research (Volume 1037)

Pages:

61-65

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1037.61

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Online since:

October 2014

Authors:

Chun Ping Pan*, Ying Lu, Yi Jun Lin

Keywords:

Dynamics Modeling, Flight Simulator, Hexapod System, Inertia, Mass

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