Aircraft Spin Recovery, with and without Thrust Vectoring, Using Nonlinear Dynamic Inversion-Reference-Cited by-同舟云学术

Aircraft Spin Recovery, with and without Thrust Vectoring, Using Nonlinear Dynamic Inversion

Published:2005-11 Issue:6 Volume:42 Page:1492-1503
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Raghavendra P. K.¹,Sahai Tuhin¹,Kumar P. Ashwani¹,Chauhan Manan¹,Ananthkrishnan N.¹

Affiliation:

1. Indian Institute of Technology Bombay, Mumbai 400 076, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.12252

Reference8 articles.

1. 1Mason, S., Stalls, Spins, and Safety, McGraw-Hill, New York, 1982.

2. 3Abzug, M. J., and Larrabee, E. E., Airplane Stability and Control-A History of the Technologies That Made Aviation Possible, Cambridge Univ. Press, Cambridge, England, U.K., 1997, pp.115-139.

3. Determination of the Spin and Recovery Characteristics of a General Aviation Design

4. Spin prediction techniques

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