Delta Operator Eigenstructure Assignment for Reconfigurable Control of a Tailless Aircraft-Reference-Cited by-同舟云学术

Delta Operator Eigenstructure Assignment for Reconfigurable Control of a Tailless Aircraft

Published:2014-11 Issue:6 Volume:37 Page:1824-1839
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Nieto-Wire Clara¹,Sobel Kenneth²

Affiliation:

1. Department of Mathematics, Hostos Community College, Bronx, New York 10451

2. Department of Electrical Engineering, The City College of New York, New York, New York 10031

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.G000036

Reference32 articles.

1. DorsettK. M.MehlD. R. “Innovative Control Effectors (ICE),” Wright Laboratory, Air Force Material Command, TR-WL-TR-96-3043, Jan. 1996.

2. DorsettK. M.FearsS. P.HouldenH. P. “Innovative Control Effectors (ICE) Phase III,” Wright Laboratory, Air Force Material Command, TR-WL-TR-3059, Aug. 1997.

3. NgoA. N.ReigelspergerW. C.BandaS. S. “Multivariable Control Law Design for a Tailless Aircraft,” AIAA Paper 1996-3866, 1996.

4. Tailless aircraft flight control using multiple time scale reconfigurable sliding modes

5. Design and Evaluation of a Damage-Tolerant Flight Control System

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