New target tracking and monitoring guidance laws for UAV

New target tracking and monitoring guidance laws for UAV

A pursuer UAV tracking and loitering around a target is the problem analyzed in this thesis. The UAV is assumed to be a fixed-wing vehicle and constant airspeed together with bounded lateral accelerations are the main constraints of the problem. Three different guidance laws are designed for ensurin...

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Bibliographic Details
Main Author: Regina, Niki <1982>
Other Authors: Bertoni, Gianni
Format: Doctoral Thesis
Language:en
Published: Alma Mater Studiorum - Università di Bologna 2011
Subjects:
ING-INF/04 Automatica
MAT/09 Ricerca operativa
Online Access:http://amsdottorato.unibo.it/3375/
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spelling ndltd-unibo.it-oai-amsdottorato.cib.unibo.it-33752014-03-24T16:29:01Z New target tracking and monitoring guidance laws for UAV Regina, Niki <1982> ING-INF/04 Automatica MAT/09 Ricerca operativa A pursuer UAV tracking and loitering around a target is the problem analyzed in this thesis. The UAV is assumed to be a fixed-wing vehicle and constant airspeed together with bounded lateral accelerations are the main constraints of the problem. Three different guidance laws are designed for ensuring a continuos overfly on the target. Different proofs are presented to demonstrate the stability properties of the laws. All the algorithms are tested on a 6DoF Pioneer software simulator. Classic control design methods have been adopted to develop autopilots for implementig the simulation platform used for testing the guidance laws. Alma Mater Studiorum - Università di Bologna Bertoni, Gianni 2011-03-29 Doctoral Thesis PeerReviewed application/pdf en http://amsdottorato.unibo.it/3375/ info:eu-repo/semantics/openAccess
collection NDLTD
language en
format Doctoral Thesis
sources NDLTD
topic ING-INF/04 Automatica
MAT/09 Ricerca operativa
spellingShingle ING-INF/04 Automatica
MAT/09 Ricerca operativa
Regina, Niki <1982>
New target tracking and monitoring guidance laws for UAV
description A pursuer UAV tracking and loitering around a target is the problem analyzed in this thesis. The UAV is assumed to be a fixed-wing vehicle and constant airspeed together with bounded lateral accelerations are the main constraints of the problem. Three different guidance laws are designed for ensuring a continuos overfly on the target. Different proofs are presented to demonstrate the stability properties of the laws. All the algorithms are tested on a 6DoF Pioneer software simulator. Classic control design methods have been adopted to develop autopilots for implementig the simulation platform used for testing the guidance laws.
author2 Bertoni, Gianni
author_facet Bertoni, Gianni
Regina, Niki <1982>
author Regina, Niki <1982>
author_sort Regina, Niki <1982>
title New target tracking and monitoring guidance laws for UAV
title_short New target tracking and monitoring guidance laws for UAV
title_full New target tracking and monitoring guidance laws for UAV
title_fullStr New target tracking and monitoring guidance laws for UAV
title_full_unstemmed New target tracking and monitoring guidance laws for UAV
title_sort new target tracking and monitoring guidance laws for uav
publisher Alma Mater Studiorum - Università di Bologna
publishDate 2011
url http://amsdottorato.unibo.it/3375/
work_keys_str_mv AT reginaniki1982 newtargettrackingandmonitoringguidancelawsforuav
_version_ 1716654322431819776

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