基于多速率卡尔曼滤波的植保无人机仿地飞行方法
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国家自然科学基金项目(51975260)、中国高校产学研创新基金项目(2021ZYB02002)和江苏高校优势学科项目(PAPD)


Terrain Following Flight for Plant Protection UAV Based on Multi-rate Kalman Filter
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    摘要:

    针对四旋翼植保无人机坡地适应性差、作业时定高精度低的问题,提出了一种融合立体视觉、气压计及惯性测量单元(IMU)的多速率卡尔曼滤波估计无人机高度的仿地飞行方法。首先基于无人机实时高度、姿态与最佳视觉检测区域之间的关系,提出了视觉检测区域自适应算法;然后融合多传感器信息建立多速率卡尔曼滤波模型用以估计无人机对地高度;最后通过自主飞行实验对无人机高度估计算法与仿地飞行方法进行验证。实验结果表明,当飞行高度为2m,飞行速度为1、2、3m/s时,植保无人机在平坦地面与15°缓坡区域均可实现高度估计平均绝对误差小于20mm,高度估计标准差小于30mm;高度控制平均绝对误差小于30mm, 高度控制标准差小于30mm;本文验证了植保无人机在地形变化场景下仿地飞行的有效性,为植保无人机在复杂地形自动化作业奠定了基础。

    Abstract:

    Aiming at the problems that the quadrotor plant protection unmanned aerial vehicle (UAV) has poor adaptability in sloping land and imprecise height measurement accuracy during operation, a terrain following flight method based on multi-rate Kalman filtering fusion of stereo vision, barometer and inertial measurement unit (IMU) information was proposed to estimate the height of UAV. Firstly, the ZED2 camera was used to obtain the binocular image of the ground below the UAV, and the point cloud information corresponding to the binocular image was calculated through the parallax principle. After analyzing the relationship between the height of the point cloud, the attitude of the UAV and the best visual detection area, an adaptive algorithm for the visual detection area was proposed to select the ground detection area. The accurate visual ground height was obtained by analyzing the point cloud data of the detection area. Secondly, a multi-rate Kalman filter model was established which fused the visual height, barometer and IMU information to estimate the height above the ground of the UAV. Finally, a two-level control system was composed of an NVIDIA microcomputer and a flight controller. The UAV’s height estimation and terrain following flight performance were verified by flight experiments. The height estimation results of remote-control flight showed that the method proposed can achieve height estimation with an absolute average error of 46.8mm and a standard deviation of 38.2mm under large height changes. The autonomous terrain following flight experiment showed that when the flight height was set to be 2m and the speed was 1m/s, 2m/s and 3m/s, respectively, no matter on the flat ground or the gentle slope of 15°, the absolute average error of height estimation was less than 20mm, and the standard deviation of height estimation was less than 30mm;the absolute average error of height control was less than 30mm, and the standard deviation of height control was less than 30mm. The research result verified the effectiveness of the plant protection UAV in the terrain changing scene, and laid a foundation for the automatic operation of the plant protection UAV in complex terrain.

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沈跃,张念,孙志伟,沈亚运,刘慧.基于多速率卡尔曼滤波的植保无人机仿地飞行方法[J].农业机械学报,2023,54(3):190-197. SHEN Yue, ZHANG Nian, SUN Zhiwei, SHEN Yayun, LIU Hui. Terrain Following Flight for Plant Protection UAV Based on Multi-rate Kalman Filter[J]. Transactions of the Chinese Society for Agricultural Machinery,2023,54(3):190-197.

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  • 收稿日期:2022-04-07
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  • 在线发布日期: 2023-03-10
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