Aircraft Autopilot Analysis and Envelope Protection for Operation Under Icing Conditions-Reference-Cited by-同舟云学术

Aircraft Autopilot Analysis and Envelope Protection for Operation Under Icing Conditions

Published:2004-05 Issue:3 Volume:27 Page:454-465
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Sharma Vikrant¹,Voulgaris Petros G.¹,Frazzoli Emilio¹

Affiliation:

1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801-2935

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/10.2514/1.1214

Reference19 articles.

1. 4Rauw, M., FDC 1.3-A SIMULINK Toolbox for Flight Dynamics and Control Analysis, 1998, available at http://www.mathworks.com/ matlabcentral/fileexchange [citedOctober 2000].

2. 5Pokhariyal, D. "Effect of Ice Accretion on Aircraft Performance and Control During Trimmed Flight," M.S. Thesis, Aeronautical and Astronautical Engineering Dept.Univ. of Illinois, Urbana, IL,2000.

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