Article ID Journal Published Year Pages File Type
708815 IFAC-PapersOnLine 2016 6 Pages PDF
Abstract

In the paper an output control approach for quad copters under the condition of the bounded input signal is presented. This algorithm is based on the high-gain principle "consecutive compensator", which was augmented by an auxiliary integral loop in order to implement the anti-windup scheme. The mathematical model describing quadcopters is decomposed on two parts: a static MIMO transformation and six SISO dynamical channels. The controller generates virtual input signals for these channels, which after inverse MIMO transformation are allocated between the actuators as real bounded control signals.

Related Topics
Physical Sciences and Engineering Engineering Computational Mechanics
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