Design and implementation of digital integration platform for airborne system

Abstract

To confront the growing difficulty along with the increasing complexity and comprehensiveness of airborne system, an airborne system integrating architecture for multiple types of models are proposed. A platform based on virtual data bus and adapters is developed. The platform’s accuracy for single model simulation is tested compared to the model’s original platform using the wind speed model of a real airplane. The platform’s integration ability, a display and control joint model containing PFD, MFD, ND, engine status collecting device, wind speed model and visualization software is established. The result shows this platform is able to efficiently integrate multiple types of models and is capable of supporting the development of complex airborne systems.

Keywords

• airborne system|virtual integration|simulation|model-based design