Application of nonlinear control strategies to aircraft at high angle of attack

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Application of nonlinear control strategies to aircraft at high angle of attack

Application of nonlinear control strategies to aircraft at high angle of attack

Huang, C.Y. / Knowles, G.J.

Nonlinear control strategies as applied to a high-alpha vehicle are discussed. The intent is to evaluate these methods for their benefit and advantage over conventional gain-scheduled linear controllers. Several techniques and their associated mechanisms are identified. The test aircraft used is the X-29, which is particularly suited for manoeuvering at a high-alpha regime. A classical linear controller designed by Grumman and NASA is used for comparison.

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Title :

Application of nonlinear control strategies to aircraft at high angle of attack

Additional title:

Die Anwendung nichtlinearer Regelungstheorien für die Flugregelung bei hohen Anstellwinkeln und hoher Geschwindigkeit

Contributors:

Huang, C.Y. (author) / Knowles, G.J. (author)

Published in:

Proceedings of the 29th IEEE Conference on Decision and Control ; 1 ; 188-193

Publication date :

1990

Size :

6 Seiten, 28 Quellen

Type of media :

Conference paper

Type of material :

Print

Language :

English

Keywords :

FLUGZEUG , REGELUNGSTECHNIK , ENTSCHEIDUNGSTHEORIE , REGELUNGSTHEORIE , LAGEREGELUNG , STABILITAET VON REGELUNGSSYSTEMEN , FLUGZEUGELEKTRONIK , FLUGREGELUNG , TRIMMEN , NASA (NATIONAL AERONAUTICS AND SPACE ADMINISTRATION) , REGELUNGSSYNTHESE

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