Robustness of dynamic inversion vs mu synthesis - Lateral-directional flight control example-Reference-Cited by-同舟云学术

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Robustness of dynamic inversion vs mu synthesis - Lateral-directional flight control example

Published:1990-08-17 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation and Control Conference
language:
Short-container-title:

Author:

ENNS DALE¹

Affiliation:

1. Honeywell Systems and Research Center; Minnesota, University, Minneapolis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-3338

Reference3 articles.

1. #define yda 0. #define ydr 5.573s-4 (define Ibeti -25.36 #define Ip -1.52 #define Ir 2.135 (define Ida 0.3347 #define Ids 0.05584 (define nbeta 5.159 #define np -0.5972 #define nr -1.935 #define nda -0.1091 Ioafznr xior -0.0143: #defir.e g 9.8 /* gravity in ds-cA2 */

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3. Attractive Manifold-Based Noncertainty-Equivalent Adaptive Control of Aircraft;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04

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