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Pressure and Shear Information based Three-Axis Attitude Control for a Micro Air Vehicle

机译:基于压力和剪切信息的微型飞行器三轴姿态控制

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Biological studies show that birds and bats can obtain airflow information with mechanoreceptors on their wing and body surfaces and use it to help achieve ultra-stable, highly maneuverable and extremely energy efficient flight. Inspired by these studies, an attitude control method for micro air vehicles (MAVs) using the flow information (pressure and shear) is studied. A nonlinear three-axis attitude dynamics model that relates the pressure and shear information to the attitude motion is developed. To tackle the flow field perception errors, measurement noises, and un-modeled dynamics, a nonlinear robust controller is implemented to track the attitude commands. A delta wing configured MAV, with forty two sensors on wing and rudder surfaces, is used as an exemplary design to validate the proposed attitude control method. The simulation results, under both steady and unsteady flow conditions, show that the proposed method can help the MAV achieving accurate and robust attitude control with small amplitudes of lateral damping.
机译:生物学研究表明,鸟类和蝙蝠可以获得机翼和体表上带有机械感受器的气流信息,并将其用于帮助实现超稳定,高度机动和极节能的飞行。受这些研究的启发,研究了一种利用流量信息(压力和剪切力)的微型飞机(MAV)的姿态控制方法。建立了将压力和切变信息与姿态运动联系起来的非线性三轴姿态动力学模型。为了解决流场感知误差,测量噪声和未建模的动力学问题,采用了非线性鲁棒控制器来跟踪姿态命令。三角翼配置的MAV在机翼和舵表面上有42个传感器,被用作示例设计来验证所提出的姿态控制方法。在稳态和非稳态流动条件下的仿真结果表明,所提出的方法可以帮助MAV在较小的侧向阻尼振幅下实现精确,鲁棒的姿态控制。

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