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PDE Boundary Control for Flexible Articulated Aircraft Wings

Paranjape, Aditya A. and Chung, Soon-Jo and Krstic, Miroslav (2011) PDE Boundary Control for Flexible Articulated Aircraft Wings. In: AIAA Guidance, Navigation, and Control Conference 2011. American Institute of Aeronautics and Astronautics (AIAA) , Reston, VA, Art. No. 2011-6486. ISBN 978-1-60086-952-5. http://resolver.caltech.edu/CaltechAUTHORS:20161222-122638313

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Abstract

The paper considers a boundary control formulation for PDEs with a system output given by a spatial integral of weighted functions of the state. This formulation is directly applicable to the control of an aircraft with articulated exible wings, in which case the output of interest is a net aerodynamic force or moment. Flexible wings can be controlled via actuation at the root or the tip. The problem of beam twist is analysed in detail to illustrate the formulation, and it shown that the control law ensures that the error between the desired output signal and the actual output signal decreases exponentially to an uniform ultimate bound. Stability of the closed loop system is proved by Lyapunov techniques. The formulation is demonstrated by simulations.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.2514/6.2011-6486DOIArticle
http://arc.aiaa.org/doi/abs/10.2514/6.2011-6486PublisherArticle
ORCID:
AuthorORCID
Chung, Soon-Jo0000-0002-6657-3907
Additional Information:© 2011 by Aditya A. Paranjape, Soon-Jo Chung and Miroslav Krstic. Published by the American Institute of Aeronautics and Astronautics, Inc. This project was supported in part by the Air Force Office of Scientific Research (AFOSR) under the Young Investigator Award Program (Grant No. FA95500910089) and the U.S. Army Research Office (ARO) under Award No W911NF-10-1-0296. The original problem of articulated wing aircraft was posed by Dr. Gregg Abate (AFRL).
Group:GALCIT
Funders:
Funding AgencyGrant Number
Air Force Office of Scientific Research (AFOSR)FA95500910089
Army Research Office (ARO)W911NF-10-1-0296
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper2011-6486
Record Number:CaltechAUTHORS:20161222-122638313
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20161222-122638313
Official Citation:Aditya Paranjape, Soon-Jo Chung, and Miroslav Krstic. "PDE Boundary Control for Flexible Articulated Aircraft Wings", AIAA Guidance, Navigation, and Control Conference, Guidance, Navigation, and Control and Co-located Conferences http://dx.doi.org/10.2514/6.2011-6486
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:73160
Collection:CaltechAUTHORS
Deposited By: Ruth Sustaita
Deposited On:23 Dec 2016 00:00
Last Modified:04 Jan 2017 19:09

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