Journal of System Simulation ›› 2018, Vol. 30 ›› Issue (10): 3732-3738.doi: 10.16182/j.issn1004731x.joss.201810017

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Design of Fault Tolerant Control Visual Simulation System For Flying Wing Aircrafts

Zhang Shaojie, Meng Qingkai   

  1. College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
  • Received:2017-05-22 Revised:2017-08-06 Online:2018-10-10 Published:2019-01-04

Abstract: A visual simulation platform based on Qt Quick was designed with respect to the simulation about fault tolerant control for flying wing aircrafts. Aircraft mathematical model and control law were developed using Simulink. Man-machine interface was developed based on Qt Quick to inject fault to Simulink model, load control law, setting up the simulation parameters and process, the interface can monitor and display graphically the key parameters to test and verify fault tolerant control laws. FlightGear visual engine was driven by MATLAB to achieve real-time visual flight simulation and the aircraft were showed in 3-D model. Baidu Map’s API function was adopted by QtWebEngineView to achieve the navigation map of the aircraft, which designed by JavaScript. The simulation results show that this simulation platform is convenient, full-featured, and scalable.

Key words: Qt Quick, fault tolerant, flying wing aircrafts, visual simulation, FlightGear, Baidu Map API

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