Design of Stable Nonlinear Pitch Control System for a Jet Aircraft by Using Artificial Intelligence-Reference-Cited by-同舟云学术

Design of Stable Nonlinear Pitch Control System for a Jet Aircraft by Using Artificial Intelligence

Published:2017-09-15 Issue:1 Volume:89 Page:57-66
ISSN:0369-8203
Container-title:Proceedings of the National Academy of Sciences, India Section A: Physical Sciences
language:en
Short-container-title:Proc. Natl. Acad. Sci., India, Sect. A Phys. Sci.

Author:

Mohanty Chandra Sekhar,Khuntia Partha Sarathi,Mitra Debjani

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy

Link

http://link.springer.com/content/pdf/10.1007/s40010-017-0396-z.pdf

Reference23 articles.

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3. Sadraey MH (2012) Aircraft design: a systems engineering approach. Wiley, London

4. Khan MA, Lu P (1994) New technique for nonlinear control of aircraft. J Guid Control Dyn 17(5):1055–1060. doi: 10.2514/3.21309

5. Hunt LR, Meyer G, Su R (1984) Nonlinear control of aircraft. In: Lecture notes in control and information sciences mathematical theory of networks and systems, vol 58, pp 463–472

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