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

Authors

Shaojie Zhang, College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China;
Qingkai Meng, College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China;

Abstract

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.

Recommended Citation

Zhang, Shaojie and Meng, Qingkai (2019) "Design of Fault Tolerant Control Visual Simulation System For Flying Wing Aircrafts," Journal of System Simulation: Vol. 30: Iss. 10, Article 17.
DOI: 10.16182/j.issn1004731x.joss.201810017
Available at: https://dc-china-simulation.researchcommons.org/journal/vol30/iss10/17

First Page

3732

Revised Date

2017-08-06

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.201810017

Last Page

3738

CLC

TP391.9

Recommended Citation

Zhang Shaojie, Meng Qingkai. Design of Fault Tolerant Control Visual Simulation System For Flying Wing Aircrafts[J]. Journal of System Simulation, 2018, 30(10): 3732-3738.

DOI

10.16182/j.issn1004731x.joss.201810017