Stabilization of uncoupled PVTOL aircraft based on a Lyapunov function-Reference-Cited by-同舟云学术

Stabilization of uncoupled PVTOL aircraft based on a Lyapunov function

Published:2011-10-10 Issue:5 Volume:34 Page:578-584
ISSN:0142-3312
Container-title:Transactions of the Institute of Measurement and Control
language:en
Short-container-title:Transactions of the Institute of Measurement and Control

Author:

Turker Turker¹,Gorgun Haulk¹,Cansever Galip¹

Affiliation:

1. Department of Control and Automation Engineering, Yildiz Technical University, Istanbul, Turkey

Abstract

In this paper we present a stabilization procedure for PVTOL (planar vertical take off and landing) aircraft with zero coupling coefficient that is defined as the effect of rolling moment on lateral acceleration. A stabilizing control structure has been designed via Lyapunov’s direct method including almost the whole state space and its asymptotic convergence has been proven using La Salle’s invariance principle. Simulation results have illustrated the effectiveness of proposed control algorithm.

Publisher

SAGE Publications

Subject

Instrumentation

Link

http://journals.sagepub.com/doi/pdf/10.1177/0142331211408638

Reference17 articles.

1. Interconnection and damping assignment passivity-based control of mechanical systems with underactuation degree one

2. Simple Tracking Controllers for Autonomous VTOL Aircraft With Bounded Inputs

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