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Disturbance observer based sliding mode control for unmanned helicopter hovering operations in presence of external disturbances

机译:基于干扰观测器的滑模控制,用于在存在外部干扰的情况下进行的无人直升机悬停操作

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Numerous control techniques are developed for miniature unmanned helicopters to do hover operation with each method having its own advantages and limitations. During the hover operation helicopters suffer from unknown external disturbances such as wind and ground effect. For a stable operation, these disturbances must be compensated accurately. This paper presents a disturbance observer based sliding mode control technique for small-scale unmanned helicopters to do hover operation in presence of external disturbances. To counteract both matched and mismatched uncertainties a new sliding surface is designed based on the disturbances estimations. The controller design is based on the linearized state-space model of the helicopter which effectively describes helicopter dynamics during the hover operations. The model mismatch and external disturbances are estimated as lumped disturbances and are compensated in the controller design. The proposed controller reduces chattering and is capable of handling matched and mismatched uncertainties. The control performance is successfully tested in Simulink.
机译:开发了用于小型无人直升机的悬停操作的多种控制技术,每种方法都有其自身的优点和局限性。在悬停操作期间,直升机遭受未知的外部干扰,例如风和地面影响。为了稳定运行,必须精确地补偿这些干扰。本文提出了一种基于干扰观测器的滑模控制技术,用于小型无人机在存在外部干扰的情况下进行悬停操作。为了抵消匹配和不匹配的不确定性,基于干扰估计设计了新的滑动表面。控制器的设计基于直升机的线性状态空间模型,该模型有效地描述了悬停操作期间的直升机动力学。模型失配和外部干扰被估计为集总干扰,并在控制器设计中得到补偿。所提出的控制器减少了抖动,并且能够处理匹配和不匹配的不确定性。控制性能已在Simulink中成功测试。

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