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Modeling and control of unmanned finless airship with robotic arms

机译:机器人武器无人垂直飞艇的建模与控制

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摘要

This paper presents the mathematical modeling and control of a finless airship that can fly at low altitudes in low wind conditions. Slow speed symmetrical airships can move freely in 3-dimensional air space with a vector propulsion system. The forces/moments of robotic arm are derived at center of gravity (CG) of the airship, and controllers are designed using classical control theory. An inner-outer loop strategy is proposed here in this paper; LQR based longitudinal and lateral controllers are designed for inner control loops while PI-based controllers are proposed for the height and velocity in outer guidance loop. The performance of the proposed scheme is validated through 6-degree of freedom nonlinear simulation having actuator dynamics and sensor models including measurement noises. Different scenarios are generated in nonlinear simulation to check the performance and robustness of the proposed scheme; simulation results validated the effectiveness of proposed scheme. (C) 2020 ISA. Published by Elsevier Ltd. All rights reserved.
机译:本文介绍了无翅膀飞艇的数学建模和控制,可以在低风条件下以低海拔飞行。缓慢速度对称飞艇可以通过矢量推进系统在三维空间中自由移动。机器人臂的力/时刻是在飞艇的重心(CG)的中心,并且控制器使用经典控制理论设计。本文提出了内部外环策略;基于LQR基纵向和横向控制器设计用于内部控制环路,而基于PI的控制器是用于外引导环中的高度和速度。通过具有致动器动力学和包括测量噪声的传感器模型的6度自由度非线性模拟来验证所提出的方案的性能。在非线性模拟中产生不同的场景,以检查所提出的方案的性能和鲁棒性;仿真结果验证了提出方案的有效性。 (c)2020 ISA。 elsevier有限公司出版。保留所有权利。

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