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基于多速率卡爾曼濾波的植保無人機(jī)仿地飛行方法
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國(guó)家自然科學(xué)基金項(xiàng)目(51975260)、中國(guó)高校產(chǎn)學(xué)研創(chuàng)新基金項(xiàng)目(2021ZYB02002)和江蘇高校優(yōu)勢(shì)學(xué)科項(xiàng)目(PAPD)


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

    針對(duì)四旋翼植保無人機(jī)坡地適應(yīng)性差、作業(yè)時(shí)定高精度低的問題,提出了一種融合立體視覺、氣壓計(jì)及慣性測(cè)量單元(IMU)的多速率卡爾曼濾波估計(jì)無人機(jī)高度的仿地飛行方法。首先基于無人機(jī)實(shí)時(shí)高度、姿態(tài)與最佳視覺檢測(cè)區(qū)域之間的關(guān)系,提出了視覺檢測(cè)區(qū)域自適應(yīng)算法;然后融合多傳感器信息建立多速率卡爾曼濾波模型用以估計(jì)無人機(jī)對(duì)地高度;最后通過自主飛行實(shí)驗(yàn)對(duì)無人機(jī)高度估計(jì)算法與仿地飛行方法進(jìn)行驗(yàn)證。實(shí)驗(yàn)結(jié)果表明,當(dāng)飛行高度為2m,飛行速度為1、2、3m/s時(shí),植保無人機(jī)在平坦地面與15°緩坡區(qū)域均可實(shí)現(xiàn)高度估計(jì)平均絕對(duì)誤差小于20mm,高度估計(jì)標(biāo)準(zhǔn)差小于30mm;高度控制平均絕對(duì)誤差小于30mm, 高度控制標(biāo)準(zhǔn)差小于30mm;本文驗(yàn)證了植保無人機(jī)在地形變化場(chǎng)景下仿地飛行的有效性,為植保無人機(jī)在復(fù)雜地形自動(dòng)化作業(yè)奠定了基礎(chǔ)。

    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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沈躍,張念,孫志偉,沈亞運(yùn),劉慧.基于多速率卡爾曼濾波的植保無人機(jī)仿地飛行方法[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),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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  • 在線發(fā)布日期: 2023-03-10
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