ass日本风韵熟妇pics男人扒开女人屁屁桶到爽|扒开胸露出奶头亲吻视频|邻居少妇的诱惑|人人妻在线播放|日日摸夜夜摸狠狠摸婷婷|制服 丝袜 人妻|激情熟妇中文字幕|看黄色欧美特一级|日本av人妻系列|高潮对白av,丰满岳妇乱熟妇之荡,日本丰满熟妇乱又伦,日韩欧美一区二区三区在线

基于MC-LADRC的水空兩棲傾轉(zhuǎn)多旋翼無(wú)人船水面起飛控制方法
CSTR:
作者:
作者單位:

作者簡(jiǎn)介:

通訊作者:

中圖分類(lèi)號(hào):

基金項(xiàng)目:

國(guó)家自然科學(xué)基金項(xiàng)目(51975260)


Surface Takeoff Control of Tilting Multi Rotor Unmanned Ship Based on MC-LADRC
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 圖/表
  • |
  • 訪(fǎng)問(wèn)統(tǒng)計(jì)
  • |
  • 參考文獻(xiàn)
  • |
  • 相似文獻(xiàn)
  • |
  • 引證文獻(xiàn)
  • |
  • 資源附件
  • |
  • 文章評(píng)論
    摘要:

    水空兩棲傾轉(zhuǎn)多旋翼無(wú)人船在多魚(yú)塘環(huán)境進(jìn)行水空跨域作業(yè)時(shí)受到復(fù)雜多變的水面流體力影響,導(dǎo)致船體姿態(tài)和飛行高度易發(fā)生較大波動(dòng)。為了提高無(wú)人船水面起飛時(shí)的姿態(tài)穩(wěn)定性,提出了一種基于模型補(bǔ)償?shù)木€(xiàn)性自抗擾水面起飛控制方法。首先對(duì)無(wú)人船多模態(tài)進(jìn)行詳細(xì)的動(dòng)力學(xué)建模;其次考慮水面起飛過(guò)程的姿態(tài)變化,建立了基于無(wú)人船實(shí)時(shí)姿態(tài)的水面張力估算模型、浮力估算模型;最后設(shè)計(jì)了基于模型補(bǔ)償?shù)木€(xiàn)性自抗擾控制器。仿真結(jié)果表明,本文方法較PID算法橫滾方向收斂時(shí)間減少66.7%,波動(dòng)減少98.3%;在無(wú)人船前進(jìn)(x軸)方向收斂時(shí)間減少34.0%;高度收斂時(shí)間減少41.2%,波動(dòng)減少80.0%。實(shí)驗(yàn)結(jié)果表明,無(wú)人船實(shí)現(xiàn)了飛行高度為1.2m時(shí),橫滾角波動(dòng)小于3°,俯仰角波動(dòng)及偏航角波動(dòng)小于2°的水面起飛。該研究提出的控制算法有效提高了水空兩棲傾轉(zhuǎn)多旋翼無(wú)人船在水空跨域過(guò)程中的安全性和抗擾能力。

    Abstract:

    The water air amphibious tilting multi rotor unmanned ships was subject to complex and variable surface fluid forces during cross domain operations in a multi fish pond environment, resulting in significant fluctuations in the ship’s attitude and flight altitude. In order to improve the attitude stability of unmanned ships during surface takeoff, a model compensation based linear self disturbance rejection surface takeoff control method was proposed. Firstly, a detailed dynamic modeling of the multimodal unmanned ship was conducted. Secondly, considering the attitude changes during the takeoff process on the water surface, a real-time attitude estimation model and buoyancy estimation model was proposed based on unmanned ships. Then, a linear self disturbance rejection attitude and altitude controller based on model compensation was designed. Finally, a linear active disturbance rejection controller based on model compensation was designed. In the simulation experiment, compared with the PID algorithm, the proposed method reduced the roll convergence time by 66.7% and the roll fluctuation by 98.3%, reduced convergence time on the x-axis by 34%, reduced convergence time on altitude by 41.2% and the fluctuation on altitude by 80.0%. The simulation results verified the effectiveness and stability of the proposed method. In practical experiments, the unmanned ship achieved takeoff from the water surface with a flying altitude of 1.2m, fluctuations of roll less than three degrees, and a fluctuation of pitch and yaw less than two degrees. The experimental results showed that the proposed control algorithm effectively improved the stability and antiinterference ability of the water air amphibious tilting multi rotor unmanned ships during the water air cross domain process.

    參考文獻(xiàn)
    相似文獻(xiàn)
    引證文獻(xiàn)
引用本文

沈躍,劉銘暉,沈亞運(yùn),劉慧.基于MC-LADRC的水空兩棲傾轉(zhuǎn)多旋翼無(wú)人船水面起飛控制方法[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),2025,56(6):608-617. SHEN Yue, LIU Minghui, SHEN Yayun, LIU Hui. Surface Takeoff Control of Tilting Multi Rotor Unmanned Ship Based on MC-LADRC[J]. Transactions of the Chinese Society for Agricultural Machinery,2025,56(6):608-617.

復(fù)制
相關(guān)視頻

分享
文章指標(biāo)
  • 點(diǎn)擊次數(shù):
  • 下載次數(shù):
  • HTML閱讀次數(shù):
  • 引用次數(shù):
歷史
  • 收稿日期:2024-03-22
  • 最后修改日期:
  • 錄用日期:
  • 在線(xiàn)發(fā)布日期: 2025-06-10
  • 出版日期:
文章二維碼