HILS based Waypoint Simulation for Fixed Wing Unmanned Aerial Vehicle (UAV)

Pub Date : 2022-11-01 DOI:10.14429/dsj.72.17952
Kaviyarasu A, Saravanakumar A, Rajesh G
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Abstract

Hardware in loop simulation HILS-based waypoint simulation for fixed wing unmanned aerial vehicles is proposed in this paper. It uses an open-source arducopter as a flight controller, mission planner, and X-plane simulator. Waypoint simulation is carried out in the flight controller and executed in an X-plane simulator through a mission planner. A fixed wing unmanned aerial vehicle with an inverted T tail configuration has been chosen to study and validate waypoint flight control algorithms. The data transmission between mission planner and flight controller is done by serial protocol, whereas data exchange between X-plane and mission planner is done by User Datagram Protocol (UDP). APM mission planner is used as a machine interface to exchange data between the flight controller and the user. User inputs and flight gain parameters, both inner loop and outer loop, can be modified with the help of a mission planner. In addition to that, the mission planner provides a visual output representation of flight data and navigation algorithm.
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基于HILS的固定翼无人机航路点仿真
提出了一种基于半实物仿真的固定翼无人机航路点仿真方法。它使用开源的arducopter作为飞行控制器、任务规划器和X平面模拟器。航路点模拟在飞行控制器中进行,并通过任务规划器在X平面模拟器中执行。选择了一种具有倒T型尾翼结构的固定翼无人机来研究和验证航路点飞行控制算法。任务规划器和飞行控制器之间的数据传输是通过串行协议完成的,而X飞机和任务规划器之间的数据交换是通过用户数据报协议(UDP)完成的。APM任务规划器用作机器接口,用于在飞行控制器和用户之间交换数据。用户输入和飞行增益参数,包括内环和外环,都可以在任务规划器的帮助下进行修改。除此之外,任务规划器还提供了飞行数据和导航算法的视觉输出表示。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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