Aircraft Flight Envelope Determination Using Upset Detection and Physical Modeling Methods-Reference-Cited by-同舟云学术

Aircraft Flight Envelope Determination Using Upset Detection and Physical Modeling Methods

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
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Author:

Keller Jeffrey¹,McKillip Robert¹,Kim Sungwan²

Affiliation:

1. Continuum Dynamics, Inc.

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6259

Reference33 articles.

1. 1Federal Aviation Administration, "Airplane Upset Recovery Training Aid, Revision 1," available from http://www.faa.gov/avr/afs/afs200/afs210/index.cfm, August 2004.

2. Application of failure detection, identification, and accommodation methods for improved aircraft safety

3. 4Shin,J.Y."ParameterTransientBehaviorAnalysisonFaultTolerantControlSystem,"NASACR-2003-212682,December 2003.

4. 5Croft,J.W."Refuse-to-crash:NASATacklesLossofControl,"AerospaceAmerica,March2003.

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