Inertia Simulation for Aircraft Braking Hardware-in-the-Loop Simulation

Feng Yu Li; Bo Li; Zong Xia Jiao

doi:10.4028/www.scientific.net/AMM.380-384.1101

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 380-384Inertia Simulation for Aircraft Braking...

Inertia Simulation for Aircraft Braking Hardware-in-the-Loop Simulation

Abstract:

In this paper, the aircraft braking simulation platform is implemented to simulate the aircraft translational energy. Considering the disadvantages of conventional facilities with fixed-mass inertia disc, such as discontinuous regulation, one novel aircraft braking simulation platform structure and inertia simulation strategy is proposed. The simulated inertia can be regulated smoothly within a specific range with the proposed method and airplanes with different inertia can be simulated on one simulation platform. Another advantage of the proposed method is that the aerodynamic drag, engine thrust and nose-wheel rolling resistance can be compensated as well. The experiment results verify the proposed method.

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Periodical:

Applied Mechanics and Materials (Volumes 380-384)

Pages:

1101-1104

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.380-384.1101

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Online since:

August 2013

Authors:

Feng Yu Li, Bo Li, Zong Xia Jiao

Keywords:

Aircraft Brake, Electric Inertia, Hardware-in-The-Loop System, Mechanical Inertia

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References

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