MATEC Web Conf.
Volume 128, 20172017 International Conference on Electronic Information Technology and Computer Engineering (EITCE 2017)
|Number of page(s)||6|
|Published online||25 October 2017|
Research and Implementation of Instrument System on a Light-Duty Electric Aircraft Simulator
School of Automation, Shenyang Aerospace University, Shenyang 110136, China
a Corresponding author: email@example.com
Considering the demands of the instrument system on a light-duty electric aircraft simulator, a semi-physical simulation instrument system, which is based on virtual reality and microcontroller technologies, is designed and implemented. Meanwhile, some key technologies are discussed and a general development method is put forward in this paper. After being completed, this simulated instrument system is connected with the flight-computing system to test its performances. The results show that it has real effect, stable operation and real time response. In practice, the instrument system not only meets the demands of the light-duty electric aircraft simulator, but also can be seen as a certain reference to develop the instrument system of other aircraft simulators.
© The authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. (http://creativecommons.org/licenses/by/4.0/).
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