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Flight-path control of a missile using the Passive Normal Form
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Vehicle Dynamics.
2005 (English)Conference paper, Published paper (Refereed)
Abstract [en]

This paper addresses the problem of controlling the flight-path angle of a missile by means of a systematic use of passivity. A simple model of a generic missile's motion in a vertical plane based on wind tunnel data is used. A variant of backstepping is introduced, based on the novel concept of Passive Normal Form, by which explicit robustness margins are obtained. The method is applied to a variety of problems, including the use of dynamical extensions.

Place, publisher, year, edition, pages
2005. 5052-5064 p.
Series
Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference, 7
Keyword [en]
Control system analysis, Data reduction, Mathematical models, Problem solving, Robustness (control systems), Wind tunnels, Flight-path control, Passive Normal Form, Wind tunnel data, Missiles
National Category
Vehicle Engineering Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-156479Scopus ID: 2-s2.0-29744432471ISBN: 1563477378 (print)ISBN: 9781563477379 (print)OAI: oai:DiVA.org:kth-156479DiVA: diva2:768542
Conference
AIAA Guidance, Navigation, and Control Conference 2005, 15-18 August 2005, San Francisco, CA, USA
Note

QC 20141204

Available from: 2014-12-04 Created: 2014-11-28 Last updated: 2014-12-04Bibliographically approved

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