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Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 1: 95 - 99

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.01.021

Development and Application of the Integrated Simulation System for a Wheeled Takeoff and Landing UAV System

  • HOU Bojiang 1, 2 ,
  • WU Yusheng 3 ,
  • ZHANG Jianfeng 2 ,
  • TIAN Xinyu 2
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  • 1 School of Marine Science and Technology,Northwestern Polytechnical University,Xi’an 710072,China
  • 2 No. 365 Institute,Northwestern Polytechnical University,Xi’an 710065,China
  • 3 No. 32204 Unit,Shaanxi Huayin 714200,China

Received date: 2020-03-25

  Online published: 2025-02-11

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Abstract

According to the requirement of actual flight tests, an integrated simulation system, which is a hardware-in-the-loop system involved the command and control system, is designed and developed for a UAV system which is taking off and landing with wheels. According to the hardware interface of sensors, the I/O interface of simulating computer is selected. Based on related experimental data, the non-linear model of the UAV considering ground taxiing is built. Then the simulation software is achieved by Matlab Simulink Real-Time. The simulation test is performed by this system for a particular flight mission. The result indicates that this system is able to perform the routine simulation and wind field cases.Furthermore, ground operators can be trained effectively by the simulation.

Key words： real-time system; unmanned aerial vehicle; integrated simulation

Cite this article

HOU Bojiang , WU Yusheng , ZHANG Jianfeng , TIAN Xinyu . Development and Application of the Integrated Simulation System for a Wheeled Takeoff and Landing UAV System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(1) : 95 -99 . DOI: 10.15892/j.cnki.djzdxb.2021.01.021

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