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一种小型无人直升机自主起飞控制方法

杜玉虎 房建成 盛蔚 雷旭升

杜玉虎, 房建成, 盛蔚, 雷旭升. 一种小型无人直升机自主起飞控制方法. 自动化学报, 2012, 38(8): 1385-1393. doi: 10.3724/SP.J.1004.2012.01385
引用本文: 杜玉虎, 房建成, 盛蔚, 雷旭升. 一种小型无人直升机自主起飞控制方法. 自动化学报, 2012, 38(8): 1385-1393. doi: 10.3724/SP.J.1004.2012.01385
DU Yu-Hu, FANG Jian-Cheng, SHENG Wei, LEI Xu-Sheng. An Automatic Take-off Method for Small-scale Unmanned Helicopters. ACTA AUTOMATICA SINICA, 2012, 38(8): 1385-1393. doi: 10.3724/SP.J.1004.2012.01385
Citation: DU Yu-Hu, FANG Jian-Cheng, SHENG Wei, LEI Xu-Sheng. An Automatic Take-off Method for Small-scale Unmanned Helicopters. ACTA AUTOMATICA SINICA, 2012, 38(8): 1385-1393. doi: 10.3724/SP.J.1004.2012.01385

一种小型无人直升机自主起飞控制方法

doi: 10.3724/SP.J.1004.2012.01385
详细信息
    通讯作者:

    杜玉虎

An Automatic Take-off Method for Small-scale Unmanned Helicopters

  • 摘要: 针对小型无人直升机(Small-scale unmanned helicopter, SUH) 起飞过程中过度依赖于地面飞行手的问题, 提出了一种基于经验知识与系统辨识的自主起飞控制方法. 首先, 通过研究专业飞行手手动操纵小型无人直升机起飞过程中高度与油门、总距舵量等信息的对应关系, 分析了利用学习飞行手的操纵行为实现小型无人直升机自主起飞的可行性, 并设计了小型无人直升机自主起飞控制流程. 引入了安全高度及变增益控制以提高自主起飞过程中的飞行安全性能, 利用不完全微分控制方法抑制了微分高频噪声. 其次, 为了获取自主起飞过程中控制参数, 采用自适应遗传算法对小型无人直升机动力学模型进行了辨识, 在动力学模型的基础上进一步辨识得到了飞行控制参数. 最后, 通过在小型无人直升机平台进行的实际飞行实验, 验证了本文方法的有效性.
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出版历程
  • 收稿日期:  2011-07-11
  • 修回日期:  2012-03-23
  • 刊出日期:  2012-08-20

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