Application of nonlinear inverse methods to the control of powered-lift aircraft over the low-speed flight envelope-Reference-Cited by-同舟云学术

Application of nonlinear inverse methods to the control of powered-lift aircraft over the low-speed flight envelope

Published:1994-01 Issue:1 Volume:59 Page:321-335
ISSN:0020-7179
Container-title:International Journal of Control
language:en
Short-container-title:International Journal of Control

Author:

FRANKLIN JAMES A.¹

Affiliation:

1. a NASA Ames Research Center , Moffett Field, CA 94035-1000, U.S.A.

Publisher

Informa UK Limited

Subject

Computer Science Applications,Control and Systems Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/00207179408923080

Reference5 articles.

1. FRANKLIN , J. A. , and ENGELLAND , S. A. , 1991 , Design and piloted simulation evaluation of integrated flight/propulsion controls for STOVL aircraft .AIAA Conference Paper 91–3108, Proceedings of the Aircraft Design Systems and Operations Meeting, Baltimore , Maryland , U.S.A.

2. Flight evaluation of augmented controls for approach and landing of powered-lift aircraft

3. STEVENS , V. C. , 1981 , A technique for determining powered-lift STOL aircraft performance at sea level from flight data at altitude .Proceedings of the AIAA Conference, Paper 81–2480.

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