基于部分传感器数据的四旋翼控制

L. Kis, B. Lantos
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引用次数: 6

摘要

微型四旋翼直升机是一个欠驱动非线性系统。通常使用几种类型的传感器来控制它。本文关注的是只有少数传感器可用的紧急情况。这些传感器主要是惯性传感器。当然,这些传感器是不够的正常机动,但控制系统应该能够水平稳定和安全着陆。提出了两种类型的控制。第一种是随机LQ状态反馈。指出了这种控制方式在实际环境中的缺点。第二种控制算法是H∞控制方法。控制设计从一个非常简单的线性模型开始。给出了线性系统的参数测量。本文的目标是处理真实系统行为中的不确定性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Quadrotor control based on partial sensor data
A miniature quadrotor helicopter is an underactuated nonlinear system. Usually several types of sensors are used to control it. This article focuses on the emergency situation, when only few sensors are available. These sensors are mainly the inertial ones. Certainly, these sensors are not enough for normal maneuvering, but the controlled system should be able for horizontal stabilization and safe landing. Two types of control are presented. The first is a casual LQ state feedback. The disadvantage of this type of control in real environment is shown. The second control algorithm is an H∞ control method. The control design starts from a very simple linear model. The parameter measurement of the linear system is shown. The goal of this article is to handle the uncertainty in the behavior of the real system.
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