Design and Implementation of Reconfigurable Flight Simulation Platform with PC

Jian Hui Xu; Sheng Jing Tang; Sheng Yi Yang

doi:10.4028/www.scientific.net/AMM.543-547.3130

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 543-547Design and Implementation of Reconfigurable Flight...

Design and Implementation of Reconfigurable Flight Simulation Platform with PC

Abstract:

In accordance with the object-oriented design principles, the flight simulation platform of each function is modular and hierarchical. The 1 Pool 2 Pieces 4 Layers software framework is proposed, using VC++ features to abstract all the replaceable modules to the same class, realizing rapid conversion of a variety of aircraft and different tests, to achieve reconfigurable. The realistic flight dynamics model considering wind disturbance is established, and with F-16 model as an example has conducted digital simulation and visual simulation. The results show that the platform has good maneuverability and fidelity, and provides reliable basis for aircraft design.

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Periodical:

Applied Mechanics and Materials (Volumes 543-547)

Pages:

3130-3135

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.543-547.3130

Citation:

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Online since:

March 2014

Authors:

Jian Hui Xu*, Sheng Jing Tang, Sheng Yi Yang

Keywords:

Hierarchical, Object-Oriented, Reconfigurable, Wind Disturbance

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* - Corresponding Author

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