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基于自適應(yīng)RBF神經(jīng)網(wǎng)絡(luò)具有模型不確定性的四旋翼無人機(jī)指定時(shí)間預(yù)設(shè)性能控制方法
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海南省重點(diǎn)研發(fā)計(jì)劃項(xiàng)目(ZDYF2024XDNY152),、廣東省企業(yè)科技特派員專項(xiàng)(GDKTP2021008500)、湛江市科技計(jì)劃項(xiàng)目(2022A105&2020A05004&2021A05194),、廣東省教育廳重點(diǎn)項(xiàng)目(2021ZDZX1041)和深圳市科技計(jì)劃項(xiàng)目(JCYJ20220530162014033)


Adaptive RBF Neural Networks for Appointed-time Performance Control of Quadcopter UAVs with Model Uncertainty
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    摘要:

    四旋翼無人機(jī)具有強(qiáng)耦合和欠驅(qū)動(dòng)的特點(diǎn),,在飛行過程中很容易受到外界干擾,進(jìn)而影響整個(gè)無人機(jī)系統(tǒng)的穩(wěn)定性和精度,。為此,,提出了一種基于RBF神經(jīng)網(wǎng)絡(luò)的指定時(shí)間預(yù)設(shè)性能約束控制策略。首先,,針對(duì)四旋翼無人機(jī)的不確定數(shù)學(xué)模型難以精確建立,,并且在執(zhí)行任務(wù)過程中存在外部未知擾動(dòng)問題,提出了一種基于指定時(shí)間預(yù)設(shè)性能控制方法,,將四旋翼無人機(jī)的軌跡跟蹤問題轉(zhuǎn)換為對(duì)位置子系統(tǒng)和姿態(tài)子系統(tǒng)的期望指令跟蹤問題,;其次,在設(shè)計(jì)控制器過程中,,為了解決“微分爆炸”問題產(chǎn)生的濾波器誤差,,引入一種新型濾波誤差補(bǔ)償方法,通過RBF神經(jīng)網(wǎng)絡(luò)逼近外部未知擾動(dòng),,并將預(yù)測(cè)結(jié)果補(bǔ)償給控制器以提高軌跡跟蹤的魯棒性,。最后,應(yīng)用仿真模擬方法驗(yàn)證無人機(jī)控制系統(tǒng)穩(wěn)定性和性能優(yōu)勢(shì),,通過飛行試驗(yàn)驗(yàn)證,,微風(fēng)聚攏環(huán)境下實(shí)際飛行軌跡與仿真模擬結(jié)果趨于一致,自主軌跡跟蹤起降位置偏差小于1cm,,證明了所提出算法的有效性,。

    Abstract:

    Quadrotor UAVs are characterized by strong coupling and underdrive, and are easily affected by external interference during flight, which in turn affects the stability and accuracy of the whole UAV system. Aiming at this problem, a specified-time preset performance constraint control policy based on RBF neural network was proposed. Firstly, in view of the difficulty of establishing an accurate mathematical model for the uncertain mathematical model of the quadrotor UAV and the existence of external unknown disturbances during the execution of the mission, a control method based on the specified time preset performance constraints was proposed, and the trajectory tracking problem of the quadrotor UAV was transformed into the desired command tracking problem for the position subsystem and the attitude subsystem;in view of the design of the controller, in order to solve the problem of the “position subsystem”, the RBF neural network was used to design the controller. Secondly, a compensation system was introduced to solve the filter error caused by the “differential explosion” problem during the controller design process. Finally, the unknown external perturbations were compensated by RBF neural network approximation and the predicted results were compensated to the controller to improve the robustness. Finally, the simulation method is used to verify the stability and performance advantages of UAV control system, flight tests were conducted to verify that the actual flight trajectory in a breeze gathering environment tended to be consistent with the simulation results. The deviation of the autonomous trajectory tracking takeoff and landing position was less than 1cm, demonstrating the effectiveness of the proposed algorithm.

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張園,鄭鴻基,劉海濤,韋麗嬌,沈德戰(zhàn),趙振華.基于自適應(yīng)RBF神經(jīng)網(wǎng)絡(luò)具有模型不確定性的四旋翼無人機(jī)指定時(shí)間預(yù)設(shè)性能控制方法[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),2024,55(4):64-73. ZHANG Yuan, ZHENG Hongji, LIU Haitao, WEI Lijiao, SHEN Dezhan, ZHAO Zhenhua. Adaptive RBF Neural Networks for Appointed-time Performance Control of Quadcopter UAVs with Model Uncertainty[J]. Transactions of the Chinese Society for Agricultural Machinery,2024,55(4):64-73.

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  • 收稿日期:2023-08-29
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  • 在線發(fā)布日期: 2024-04-10
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