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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Veröffentlicht in:Asian journal of control 2014-11, Vol.16 (6), p.1849-1858
Hauptverfasser: Gandolfo, D., Rosales, C., Patiño, D., Scaglia, G., Jordan, M.
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container_end_page 1858
container_issue 6
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container_title Asian journal of control
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creator Gandolfo, D.
Rosales, C.
Patiño, D.
Scaglia, G.
Jordan, M.
description 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.
doi_str_mv 10.1002/asjc.819
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source Wiley Online Library Journals Frontfile Complete
subjects Aerospace engineering
Aircraft
internal states
Linear algebra
linear algebra based controller
Markov propriety
PVTOL aircraft
Theory
Tracking control systems
tracking error
title Trajectory Tracking Control of a PVTOL Aircraft Based on Linear Algebra Theory
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