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基于深度學(xué)習的四旋翼無(wú)人機控制系統設計
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武警工程大學(xué)信息工程學(xué)院

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2018年度裝備軍內科研項目:無(wú)人機態(tài)勢預測感知在處置群體性事件中的應用研究(WJ20182A020020-2); ?2019年大學(xué)基礎研究基金項目:基于智能視覺(jué)的群體性時(shí)間現場(chǎng)態(tài)勢感知與預警方法研究(WJY201906); ?武警部隊軍事理論研究計劃課題立項:基于智能視頻分析的大規模群體性事件現場(chǎng)態(tài)勢感知與預警方法研究(WJJY19-134)


Design of Quadrotor UAV Control System Based on Deep Learning
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    摘要:

    針對傳統四旋翼無(wú)人機控制系統受到外界干擾,無(wú)法及時(shí)躲避障礙物而導致控制精準度低的問(wèn)題,提出了基于深度學(xué)習的四旋翼無(wú)人機控制系統設計。根據四旋翼無(wú)人機控制系統總體結構,加入超聲波測距模塊。依據系統硬件框圖,采用TMS320F28335型號主控芯片,實(shí)現關(guān)鍵態(tài)勢智能分析。以串級 PID 控制器的控制對象為無(wú)人機姿態(tài)角度,控制電機轉速。根據DSP發(fā)出不同占空比的PWM信號,改變無(wú)人機飛行姿態(tài),依據執行機構驅動(dòng)原理,保證無(wú)人機飛行時(shí)的平衡狀態(tài)。使用紅外遙控系統,應用編/解碼操控集成電路芯片,采用TS0P1738型號紅外線(xiàn)接收器,適合于紅外線(xiàn)遙控數據傳輸。構建深度學(xué)習目標控制模型,利用處突陣法與三角形相似原理,計算像素尺寸,獲取障礙物距無(wú)人機當前位置距離,避免受到外界障礙物干擾。自適應擴展Kalman濾波器技術(shù)對無(wú)人機自動(dòng)控制系統有效減小測量誤差,準確地對機動(dòng)目標進(jìn)行追蹤。由系統調試結果可知,該系統控制的俯仰角、航向角、橫滾角與實(shí)際值一致,對處理突發(fā)性群體事件具有重要意義。

    Abstract:

    In order to solve the problem that the control system of traditional four rotor UAV is disturbed by the outside world and can't avoid the obstacles in time, which leads to the low control accuracy, the control system design of four rotor UAV Based on deep learning is proposed. According to the overall structure of the four rotor UAV control system, the ultrasonic ranging module is added. According to the system hardware block diagram, TMS320F28335 main control chip is used to realize the key situation intelligent analysis. Taking the control object of the cascade PID controller as the attitude angle of the UAV, the motor speed is controlled. According to the PWM signals of different duty cycle sent by DSP, the flight attitude of UAV is changed, and according to the driving principle of actuator, the balance state of UAV during flight is ensured. Using infrared remote control system, using encoder / decoder to control IC chip, using ts0p1738 infrared receiver, suitable for infrared remote control data transmission. The depth learning target control model is constructed, and the pixel size is calculated by using the method of location matrix and the principle of triangle similarity. The distance between the obstacle and the current position of UAV is obtained to avoid the interference of external obstacles. The adaptive extended Kalman filter technology can effectively reduce the measurement error of UAV automatic control system and accurately track the maneuvering target. According to the results of system debugging, the pitch angle, heading angle and roll angle controlled by the system are consistent with the actual values, which is of great significance to deal with unexpected group events.

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徐一鳴,李笑,楊凱凱,楊宇.基于深度學(xué)習的四旋翼無(wú)人機控制系統設計計算機測量與控制[J].,2020,28(5):123-127.

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  • 收稿日期:2020-03-03
  • 最后修改日期:2020-04-01
  • 錄用日期:2020-04-01
  • 在線(xiàn)發(fā)布日期: 2020-05-25
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