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Flight control simulations of a butterfly-like flapping wing-body model by the immersed boundary-lattice Boltzmann method

机译:浸入式边界格子Boltzmann方法对蝴蝶状扑翼机体模型的飞行控制仿真

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摘要

Flapping flight of insects and bio-inspired micro air vehicles requires not only the generation of aerodynamic forces for supporting the weight against gravity and for driving forward, but also the flight control for maintaining the balance while flying. In this study, we investigate the flight control of a butterfly like flapping wing-body model numerically by using the immersed boundary-lattice Boltzmann method. First, we simulate the control of a pitching motion by moving a weight along the body. It is found that the pitching angle can be controlled by determining the position of the weight with a P control scheme. Second, we simulate the control of a rolling motion from a large initial disturbance on the rolling angle by moving a weight perpendicular to the body. It is found that the rolling angle can be controlled by determining the position of the weight with a PI control scheme. Finally, we simulate the control of a pitching motion by interrupting the wing motion shortly at the top and/or the bottom dead centers of the wing motion. It is found that the pitching angle is controlled by determining the interval of the interruption with a PID control scheme. In addition, it is found that the present control works well even for a large disturbance. (C) 2016 Elsevier Ltd. All rights reserved.
机译:昆虫和受生物启发的微型飞行器的扑翼飞行不仅需要产生空气动力来支撑配重抵抗重力并向前行驶,还需要飞行控制来保持飞行时的平衡。在这项研究中,我们通过使用浸没边界格子Boltzmann方法数值研究了蝴蝶状扑翼机体模型的飞行控制。首先,我们通过沿着身体移动重物来模拟俯仰运动的控制。发现可以通过使用P控制方案确定配重的位置来控制俯仰角。其次,我们通过垂直于车身移动重物来模拟对滚动角产生较大初始干扰的滚动运动控制。发现可以通过使用PI控制方案确定配重的位置来控制滚动角。最后,我们通过在机翼运动的顶部和/或下止点不久中断机翼运动来模拟俯仰运动的控制。发现俯仰角是通过利用PID控制方案确定中断间隔来控制的。另外,发现即使对于较大的干扰,本控制也能很好地工作。 (C)2016 Elsevier Ltd.保留所有权利。

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