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基于视惯融合的无人飞行器导航数据仿真方法
作者姓名:张逸舟  曾庆化  许 睿  王景琪  罗怡雪
作者单位:南京航空航天大学自动化学院 导航研究中心;南京航空航天大学自动化学院 导航研究中心; 南京航空航天大学 先进飞行器导航、控制与健康管理工业和信息化部重点实验室; 南京航空航天大学 江苏省物联网与控制技术重点实验室
基金项目:国家自然科学基金资助项目(61533008, 61603181)
摘    要:无人飞行器在卫星信号拒止情况下难以获得较高的导航精度。为此,需要研究基于载体自身传感设备的自主导航定位方法。立足于飞行器平台的视觉惯性紧耦合算法架构VINS-Mono,提出并设计了一种视觉惯性数据仿真方法,针对匀速直线运动过程无法恢复视觉尺度的问题,进行了初始化运动轨迹补充。仿真研究结果表明,该方法所补充的轨迹能够很好地对齐视觉与惯性信息并恢复尺度,实现导航参数的正确求解。理想条件下500m平飞范围内定位误差占比不超过真值的3.5%,可作为评估卫星拒止环境下无人飞行器视觉惯性组合导航性能的参考方案。

关 键 词:无人飞行器  卫星信号拒止  VINS-Mono  初始化  仿真方法

Data Simulation Method of UAV Navigation on Visual-Inertial Fusion
Authors:ZHANG Yizhou  ZENG Qinghu  XU Rui  WANG Jingqi  LUO Yixue
Institution:College of Automation Engineering, Navigation Research Center, Nanjing University of Aeronautics and Astronautics;;College of Automation Engineering, Navigation Research Center, Nanjing University of Aeronautics and Astronautics; Key Laboratory of Navigation, Guidance and Health-management Technologies of Advanced Aerocraft, Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics; Jiangsu Key Laboratory of Internet of Things and Control Technology, Nanjing University of Aeronautics and Astronautics
Abstract:It is hard for UAVs to obtain high navigation accuracy under the condition of satellite signal rejection. Therefore, studying the autonomous navigation and positioning method with sensing equipment is significant. Based on the tightly coupled visual inertia algorithm architecture VINS-Mono on aircraft platforms, a visual-inertial data simulation method is proposed in this paper. The initial motion trajectory is supplemented for solving problems that the visual scale cannot be restored in uniform linear motion. The simulation experiment results show that the navigation parameters and the scale can be correctly solved by adding the trajectory for the alignment of visual and inertial information. Under ideal conditions, the positioning error within 500m is less than 3.5% of the true value, which provides an important algorithm reference for UAV visual-inertial integrated navigation in this scene.
Keywords:UAV  satellite signal rejection  VINS-Mono  initialization  simulation method
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