LPV modeling of guided projectiles for terminal guidance

Spilios Theodoulis, Yannick Morel, Philippe Wernert, Antonios Tzes

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This article presents a detailed study concerning the equilibrium analysis and the linear parameter-varying (LPV) modeling of the six degrees-of-freedom (6DoF) nonlinear model of a fin-guided, gun-launched projectile. The equilibrium manifold of the system is obtained through a minimal vector of parameters characterizing its flight envelope and a maneuverability analysis involving the attainable vertical acceleration is presented. In the following, an analytic linear parameter varying model of the airframe yaw/pitch axes is derived and several issues concerning its scope and internal structure are discussed. Finally, an application of these results on a single trajectory point is performed and the resulting linear time-invariant (LTI) model is analyzed in terms of pole/zero location and internal stability.

Original languageEnglish (US)
Title of host publication18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings
Pages1455-1460
Number of pages6
DOIs
StatePublished - Sep 29 2010
Event18th Mediterranean Conference on Control and Automation, MED'10 - Marrakech, Morocco
Duration: Jun 23 2010Jun 25 2010

Other

Other18th Mediterranean Conference on Control and Automation, MED'10
CountryMorocco
CityMarrakech
Period6/23/106/25/10

Fingerprint

Projectiles
Flight envelopes
Maneuverability
Airframes
Poles
Trajectories

ASJC Scopus subject areas

  • Control and Systems Engineering

Cite this

Theodoulis, S., Morel, Y., Wernert, P., & Tzes, A. (2010). LPV modeling of guided projectiles for terminal guidance. In 18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings (pp. 1455-1460). [5547843] https://doi.org/10.1109/MED.2010.5547843

LPV modeling of guided projectiles for terminal guidance. / Theodoulis, Spilios; Morel, Yannick; Wernert, Philippe; Tzes, Antonios.

18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings. 2010. p. 1455-1460 5547843.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Theodoulis, S, Morel, Y, Wernert, P & Tzes, A 2010, LPV modeling of guided projectiles for terminal guidance. in 18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings., 5547843, pp. 1455-1460, 18th Mediterranean Conference on Control and Automation, MED'10, Marrakech, Morocco, 6/23/10. https://doi.org/10.1109/MED.2010.5547843
Theodoulis S, Morel Y, Wernert P, Tzes A. LPV modeling of guided projectiles for terminal guidance. In 18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings. 2010. p. 1455-1460. 5547843 https://doi.org/10.1109/MED.2010.5547843
Theodoulis, Spilios ; Morel, Yannick ; Wernert, Philippe ; Tzes, Antonios. / LPV modeling of guided projectiles for terminal guidance. 18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings. 2010. pp. 1455-1460
@inproceedings{1752ff3d83514020964923e4ac4bd9f5,
title = "LPV modeling of guided projectiles for terminal guidance",
abstract = "This article presents a detailed study concerning the equilibrium analysis and the linear parameter-varying (LPV) modeling of the six degrees-of-freedom (6DoF) nonlinear model of a fin-guided, gun-launched projectile. The equilibrium manifold of the system is obtained through a minimal vector of parameters characterizing its flight envelope and a maneuverability analysis involving the attainable vertical acceleration is presented. In the following, an analytic linear parameter varying model of the airframe yaw/pitch axes is derived and several issues concerning its scope and internal structure are discussed. Finally, an application of these results on a single trajectory point is performed and the resulting linear time-invariant (LTI) model is analyzed in terms of pole/zero location and internal stability.",
author = "Spilios Theodoulis and Yannick Morel and Philippe Wernert and Antonios Tzes",
year = "2010",
month = "9",
day = "29",
doi = "10.1109/MED.2010.5547843",
language = "English (US)",
isbn = "9781424480920",
pages = "1455--1460",
booktitle = "18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings",

}

TY - GEN

T1 - LPV modeling of guided projectiles for terminal guidance

AU - Theodoulis, Spilios

AU - Morel, Yannick

AU - Wernert, Philippe

AU - Tzes, Antonios

PY - 2010/9/29

Y1 - 2010/9/29

N2 - This article presents a detailed study concerning the equilibrium analysis and the linear parameter-varying (LPV) modeling of the six degrees-of-freedom (6DoF) nonlinear model of a fin-guided, gun-launched projectile. The equilibrium manifold of the system is obtained through a minimal vector of parameters characterizing its flight envelope and a maneuverability analysis involving the attainable vertical acceleration is presented. In the following, an analytic linear parameter varying model of the airframe yaw/pitch axes is derived and several issues concerning its scope and internal structure are discussed. Finally, an application of these results on a single trajectory point is performed and the resulting linear time-invariant (LTI) model is analyzed in terms of pole/zero location and internal stability.

AB - This article presents a detailed study concerning the equilibrium analysis and the linear parameter-varying (LPV) modeling of the six degrees-of-freedom (6DoF) nonlinear model of a fin-guided, gun-launched projectile. The equilibrium manifold of the system is obtained through a minimal vector of parameters characterizing its flight envelope and a maneuverability analysis involving the attainable vertical acceleration is presented. In the following, an analytic linear parameter varying model of the airframe yaw/pitch axes is derived and several issues concerning its scope and internal structure are discussed. Finally, an application of these results on a single trajectory point is performed and the resulting linear time-invariant (LTI) model is analyzed in terms of pole/zero location and internal stability.

UR - http://www.scopus.com/inward/record.url?scp=77956988594&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=77956988594&partnerID=8YFLogxK

U2 - 10.1109/MED.2010.5547843

DO - 10.1109/MED.2010.5547843

M3 - Conference contribution

AN - SCOPUS:77956988594

SN - 9781424480920

SP - 1455

EP - 1460

BT - 18th Mediterranean Conference on Control and Automation, MED'10 - Conference Proceedings

ER -