Trajectory Tracking Control of a PVTOL Aircraft Based on Linear Algebra Theory

In this work, a trajectory tracking control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft using linear algebra theory. The resulting control law is implemented easily since the equation to be solved is not complex. The tracking is achieved providing convergence of t...

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Bibliographic Details
Authors: Gandolfo, Daniel, Rosales, Claudio Dario, Patiño, Héctor Daniel, Scaglia, Gustavo Juan Eduardo, Jordan, Mario Alberto
Format: article
Status:Published version
Publication Date:2014
Country:Argentina
Institution:Consejo Nacional de Investigaciones Científicas y Técnicas
Repository:CONICET Digital (CONICET)
Language:English
OAI Identifier:oai:ri.conicet.gov.ar:11336/12563
Online Access:http://hdl.handle.net/11336/12563
Access Level:Open access
Keyword:Pvtol Aircraft
Markov Propriety
Linear Algebra Based Controller
Internal States
Tracking Error
https://purl.org/becyt/ford/2.2
https://purl.org/becyt/ford/2
Description
Summary:In this work, a trajectory tracking control design is proposed for the planar vertical takeoff and landing (PVTOL) aircraft using linear algebra theory. The resulting control law is implemented easily since the equation to be solved is not complex. The tracking is achieved providing convergence of the tracking errors to zero, and simulation results show the good performance of the proposed controller.

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