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Performance and Stability of an Agile Tail-less MAV with Flexible Articulated Wings

Paranjape, Aditya and Chakravarthy, Animesh and Chung, Soon-Jo and Hilton, Harry H. (2010) Performance and Stability of an Agile Tail-less MAV with Flexible Articulated Wings. In: AIAA Atmospheric Flight Mechanics Conference 2010. American Institute of Aeronautics and Astronautics , Reston, VA, Art. No. 2010-7937. ISBN 978-1-62410-151-9. http://resolver.caltech.edu/CaltechAUTHORS:20161222-121459009

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Abstract

This paper considers the problems of (a) modelling the ight mechanics of a tail-less MAV equipped with exible articulated wings, and (b) the analysis of its turning performance. The wings are assumed to have two degrees of freedom - heave and twist. They are assumed to be actuated from the root, which is the abstraction of an experimental control mechanism being developed by the authors. The dihedral and twist angles at the wing root are controlled. A novel actuator concept of axial tension to control wing stiffness has been explored in this paper. It is shown that axial tension in the wing has a significant effect on the turning performance of the aircraft, although the effect is not uniformly beneficial in nature. The effect of exibility on the steady state turning performance of the aircraft has been demonstrated by comparing it with that of a rigid aircraft, and with that of a similar aircraft possessing a wing with different elastic properties.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.2514/6.2010-7937DOIArticle
http://arc.aiaa.org/doi/abs/10.2514/6.2010-7937PublisherArticle
ORCID:
AuthorORCID
Chung, Soon-Jo0000-0002-6657-3907
Additional Information:© 2010 American Institute of Aeronautics and Astronautics. This project was supported by the Air Force Office of Scientific Research (AFOSR) under the Young Investigator Award Program (Grant No. FA95500910089) monitored by Dr. W. Larkin. The original problem was posed by Dr. Gregg Abate (AFRL). This paper also benefitted from stimulating discussions with Mr. Johnny Evers (AFRL).
Group:GALCIT
Funders:
Funding AgencyGrant Number
Air Force Office of Scientific Research (AFOSR)FA95500910089
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper2010-7937
Record Number:CaltechAUTHORS:20161222-121459009
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20161222-121459009
Official Citation:Aditya Paranjape, Animesh Chakravarthy, Soon-Jo Chung, and Harry Hilton. "Performance and Stability of an Agile Tail-less MAV with Flexible Articulated Wings", AIAA Atmospheric Flight Mechanics Conference, Guidance, Navigation, and Control and Co-located Conferences http://dx.doi.org/10.2514/6.2010-7937
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:73159
Collection:CaltechAUTHORS
Deposited By: Ruth Sustaita
Deposited On:23 Dec 2016 00:03
Last Modified:04 Jan 2017 19:05

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