Basic Simulations of Kinodynamic Control Using Local Environmental Information

K. Motonaka, Keigo Watanabe
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Abstract

—The kinodynamic control aims to design a control input so that we consider kinematic constraints, which is generated from an environment, and dynamic constraints of the airframe, simultaneously. In the previous research, we converted the environmental information to the harmonic potential field (HPF), and added its gradient information to the conventional dynamical control input. However, it was assumed in the previous research that the environmental information is known absolutely. In this research, we assume the actual situation that the quadrotor flies autonomously in an indoor environment. We propose the kinodynamic control that considers the measurable region of the sensor mounted on the quadrotor to obtain the environmental information. In this paper, we make a basic simulation experiment and confirm that the proposed control input works well.
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基于局部环境信息的动力学控制基本仿真
动力学控制的目的是设计一个控制输入,使我们同时考虑由环境产生的运动学约束和机体的动力学约束。在之前的研究中,我们将环境信息转换为谐波势场(HPF),并将其梯度信息添加到传统的动态控制输入中。然而,在之前的研究中,假设环境信息是绝对已知的。在本研究中,我们假设四旋翼飞行器在室内环境中自主飞行的实际情况。提出了一种考虑传感器可测区域的四旋翼飞行器动力学控制方法来获取环境信息。在本文中,我们做了一个基本的仿真实验,并证实了所提出的控制输入效果良好。
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