Nonlinear command augmentation system for a high performance aircraft-Reference-Cited by-同舟云学术

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Nonlinear command augmentation system for a high performance aircraft

Published:1993-08-09 Issue: Volume: Page:
ISSN:
Container-title:Guidance, Navigation and Control Conference
language:
Short-container-title:

Author:

MENON R.¹

Affiliation:

1. Optimal Synthesis, Palo Alto, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3777

Reference21 articles.

1. Meyer, G., and Cicolani, L. "Applicationof Nonlinear SystemInverses to AutomaticFlight Control Design - System Concepts and Flight Evaluations,"AGARDograph 251onTheoryand Applications of Optimal Control in Aerospace Systems, 1980.

2. Nonlinear flight test trajectory controllers for aircraft

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