某滑跑型无人机综合仿真系统开发与应用  

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

作　　者：侯泊江 吴玉生 张剑锋[2] 田心宇[2] HOU Bojiang;WU Yusheng;ZHANG Jianfeng;TIAN Xinyu(School of Marine Science and Technology,Northwestern Polytechnical University,Xi’an 710072,China;No.365 Institute,Northwestern Polytechnical University,Xi’an 710065,China;No.32204 Unit,Shaanxi Huayin 714200,China)

机构地区：[1]西北工业大学航海学院,西安710072 [2]西北工业大学第365研究所,西安710065 [3]32204部队,陕西华阴714200

出　　处：《弹箭与制导学报》2021年第1期95-99,共5页Journal of Projectiles,Rockets,Missiles and Guidance

基　　金：陕西省重点产业创业链(群)项目(2019ZDLGY14-06)资助。

摘　　要：针对外场飞行试验需求,设计并研制了一种指挥控制系统在环的无人机综合仿真系统。通过分析机载传感器硬件接口,构建了仿真平台硬件框架并完成了设备选型。基于相关试验数据,构建了考虑地面滑行的无人机非线性数学模型,并在Simulink Real-Time环境下开发了实时仿真模型和仿真软件。针对某次飞行任务进行了仿真试验,结果表明,该系统不仅能进行常规流程和风干扰环境下的飞行仿真,还可以针对具体任务对操纵手进行模拟训练。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.

关 键 词：实时系统 无人机 综合仿真 

分 类 号：V211[航空宇航科学与技术—航空宇航推进理论与工程] V249.4