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基于貝葉斯改進(jìn)神經(jīng)網(wǎng)絡(luò )的電力無(wú)人機魯棒姿態(tài)控制方法
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Robust attitude control method of electric UAV based on Bayesian improved neural network
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    摘要:

    針對電力無(wú)人機在工作狀態(tài)下受到外部因素干擾、無(wú)法精準控制運動(dòng)姿態(tài)的問(wèn)題,提出基于貝葉斯改進(jìn)神經(jīng)網(wǎng)絡(luò )的電力無(wú)人機魯棒姿態(tài)控制方法。綜合考慮電力無(wú)人機的組成結構、運動(dòng)以及動(dòng)力原理,構建電力無(wú)人機數學(xué)模型。利用傳感器設備檢測電力無(wú)人機的實(shí)時(shí)位姿,采用飛行路線(xiàn)規劃的方式確定姿態(tài)控制目標。在考慮風(fēng)場(chǎng)威脅條件和故障狀態(tài)的情況下,利用貝葉斯改進(jìn)神經(jīng)網(wǎng)絡(luò )計算無(wú)人機的姿態(tài)控制量,以魯棒姿態(tài)控制器作為硬件支持,實(shí)現魯棒姿態(tài)控制。通過(guò)性能測試得出結論:優(yōu)化設計方法的姿態(tài)角控制誤差始終低于0.2°,且在三種不同風(fēng)場(chǎng)工況下,控制誤差的波動(dòng)程度不高于0.5°,與傳統方法相比,優(yōu)化設計方法在姿態(tài)控制精度和魯棒性方面具有明顯優(yōu)勢。

    Abstract:

    Aiming at the problem that the electric UAV cannot precisely control its motion attitude due to the interference of external factors, a robust attitude control method based on Bayesian improved neural network was proposed for electric UAV. The mathematical model of electric UAV is established by considering the composition, motion and dynamic principle of electric UAV. The sensor equipment is used to detect the real-time pose of the electric UAV and the attitude control target is determined by the way of flight path planning. Considering the wind threat condition and fault state, the attitude control quantity of UAV is calculated by using Bayesian improved neural network, and the robust attitude controller is used as the hardware support to realize the robust attitude control. Through the performance test, it is concluded that the attitude Angle control error of the optimized design method is always lower than 0.2°, and the fluctuation degree of the control error is no more than 0.5° under three different wind conditions. Compared with the traditional method, the optimized design method has obvious advantages in the accuracy and robustness of attitude control.

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嚴永鋒,任濤,王濤,吳烜,吳琳.基于貝葉斯改進(jìn)神經(jīng)網(wǎng)絡(luò )的電力無(wú)人機魯棒姿態(tài)控制方法計算機測量與控制[J].,2024,32(2):142-148.

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歷史
  • 收稿日期:2023-06-15
  • 最后修改日期:2023-07-24
  • 錄用日期:2023-07-24
  • 在線(xiàn)發(fā)布日期: 2024-03-20
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