MEMS based navigation and control of a nonlinear quadrotor with tiltable rotors

G. Scholz, K. Müller, G. Trommer
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引用次数: 1

Abstract

The support of rescue forces using Micro Aerial Vehicles (MAVs) is a challenging task which is addressed in this work. In order to fulfill this task an advanced type of MAV is being developed: A quadrotor with tiltable rotors. This vehicle is able to perform vertical takeoff and landing maneuvers as well as to control attitude and velocity independently. To achieve this goal the navigation filter fuses the information of a micro electrical mechanical system inertial measurement unit (MEMS IMU) with data provided by a laser range finder. A stochastic cloning Kalman filter is used to perform the data fusion appropriately. To control this new kind of vehicle a nonlinear controller is used. The controller is separated into a common backstepping controller and a control allocation unit. The performance of the system is demonstrated by simulations based on model identification of real sensors and hardware.
基于MEMS的非线性可倾四旋翼导航与控制
使用微型飞行器(MAVs)支持救援部队是一项具有挑战性的任务,这在本工作中得到了解决。为了完成这项任务,一种先进的MAV正在开发中:一种带有可倾斜旋翼的四旋翼。这种飞行器能够进行垂直起降机动,并能独立控制姿态和速度。为了实现这一目标,导航滤波器将微机电系统惯性测量单元(MEMS IMU)的信息与激光测距仪提供的数据融合在一起。采用随机克隆卡尔曼滤波器进行数据融合。为了控制这种新型车辆,采用了非线性控制器。所述控制器分为公共后退控制器和控制分配单元。通过对实际传感器和硬件的模型识别,验证了系统的性能。
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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