Guidance and Control of an Airplane under Severe Structural Damage-Reference-Cited by-同舟云学术

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Guidance and Control of an Airplane under Severe Structural Damage

Published:2010-04-20 Issue: Volume: Page:
ISSN:
Container-title:AIAA Infotech@Aerospace 2010
language:
Short-container-title:

Author:

Johnson Eric¹,Chowdhary Girish¹,Kimbrel M.¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3342

Reference14 articles.

1. 1040 1050 1060 1070 1080 1090 1100 1110 1120 1130 -0.5 angular rate data corrected for bias

2. 1040 1050 1060 1070 1080 1090 1100 1110 1120 1130 -0.2 0 0.2 0.4 0.6

3. 1040 1050 1060 1070 1080 1090 1100 1110 1120 1130 -1

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5. Simulation of a high-agility model airplane in the presence of severe structural damage and failures, and design of a dynamic inversion controller;CEAS Aeronautical Journal;2011-08-27

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