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小型無人直升機航向線性自抗擾控制
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國家自然科學基金青年基金項目(51405209)


Linear Active Disturbance Rejection Control for Yaw Channel of Small-scale Unmanned Helicopter
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    摘要:

    針對小型無人直升機航向系統(tǒng)存在內(nèi)部不確定性和外部擾動大的問題,提出了一種基于線性自抗擾控制(LADRC)算法來實現(xiàn)航向通道高性能控制方法。首先,分析和推導(dǎo)了Trex—600型無人直升機的航向模型,并引入陣風模型模擬實際飛行環(huán)境。然后,根據(jù)LADRC的控制原理設(shè)計了基于二階LADRC的航向控制系統(tǒng),并利用人工蜂群算法對控制器參數(shù)進行了整定。最后,對所設(shè)計的控制策略進行了仿真分析與實驗驗證,實現(xiàn)了無人直升機航向通道的軌跡跟蹤控制,并與常見的PID控制進行了比較。結(jié)果表明:設(shè)計的LADRC控制器魯棒性好、響應(yīng)時間快、控制精度高,能夠使Trex—600型無人直升機的航向角快速、精確地跟蹤參考軌跡。

    Abstract:

    Small-scale unmanned helicopter has a peculiar flight feature of vertically take-off and landing, fixed position hovering, flying in low velocity, forward flight, rearward flight and so on. It is mainly used for civilian and military field with the advantage of light weight, low price and small scale. However, the small-scale unmanned helicopter is a strong coupled, under actuated, multivariable, time varying, open-loop unstable and high order nonlinear system. It is a great challenge to realize the research of its autonomous flight. Aiming at the internal uncertainties and large disturbance of the small-scale unmanned helicopter, a controller for yaw channel based on linear active disturbance rejection controller (LADRC) was proposed to realize the high performance control. Firstly, the yaw model of Trex—600 unmanned helicopter was analyzed and deduced, and the gust model was introduced to simulate the actual flight environment. Then, the principle of LADRC was elaborated and the yaw control system was designed based on LADRC of second order. In order to obtain the appropriate control parameters, the novel artificial bee colony algorithm was applied to conduct parameters tuning. Lastly, a trajectory tracking simulation and experiment were used to test the proposed controller compared with the PID controller. The results showed that the LADRC controller had the ability of good robustness, fast response and high control precision. The yaw angle of the Trex—600 unmanned helicopter can track the referenced trajectory fleetly and accurately.

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丁力,馬瑞,單文桃,吳洪濤.小型無人直升機航向線性自抗擾控制[J].農(nóng)業(yè)機械學報,2017,48(5):22-27. DING Li, MA Rui, SHAN Wentao, WU Hongtao. Linear Active Disturbance Rejection Control for Yaw Channel of Small-scale Unmanned Helicopter[J]. Transactions of the Chinese Society for Agricultural Machinery,2017,48(5):22-27.

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  • 收稿日期:2016-08-25
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  • 在線發(fā)布日期: 2017-05-10
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