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首页> 外文期刊>Transactions of the Institute of Measurement and Control >Command-filtered backstepping control for a multi-vectored thrust stratospheric airship
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Command-filtered backstepping control for a multi-vectored thrust stratospheric airship

机译:多矢量平流层飞艇的命令过滤后推控制

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摘要

A stratospheric airship is an airship flying at a high altitude of 20km as a stratospheric platform. Due to the low atmospheric density and flight speed, the efficiency of a conventional actuator, such as an aerodynamic control surface, is decreased. Thus, a new multi-vectored thrust airship called a flat peach is discussed in this paper. This article describes the derivation, design and simulation implementation of a non-linear controller for an airship with multi-vector thrust. The controller is designed using a command-filtered, vector backstepping approach, and can set the airship track three Cartesian positions (x,y,z) and yaw angle to their desired values and stabilize the pitch and roll angles. The controller is non-linear to address the kinematics and airship dynamics. The approach guarantees exponential stability of a compensated tracking error in the sense of Lyapunov. Both the stability analysis and simulation results are included.
机译:平流层飞艇是作为平流层平台在20公里高空飞行的飞艇。由于低的大气密度和飞行速度,传统致动器例如空气动力控制表面的效率降低。因此,本文讨论了一种新型的多矢量推力飞艇,称为扁平桃子。本文介绍了具有多矢量推力的飞艇的非线性控制器的推导,设计和仿真实现。该控制器采用命令过滤的矢量后推方法进行设计,可以将飞艇的三个笛卡尔位置(x,y,z)和偏航角设置为其所需值,并稳定俯仰和侧倾角。控制器是非线性的,以解决运动学和飞艇动力学问题。该方法在Lyapunov的意义上保证了补偿跟踪误差的指数稳定性。包括稳定性分析和仿真结果。

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