Robust integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques-Reference-Cited by-同舟云学术

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Robust integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques

Published:1993-01 Issue:1 Volume:29 Page:129-145
ISSN:0005-1098
Container-title:Automatica
language:en
Short-container-title:Automatica

Author:

Garg Sanjay

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Control and Systems Engineering

Reference22 articles.

1. Simulation development for U.S./Canada controls technology program;Akhter,1989

2. Military specification—flying qualities of piloted V/STOL aircraft,1970

3. Structured stability robustness improvement by eigenspace assignment techniques: A hybrid methodology;Apkarian;J. of Guidance, Control and Dynamics,1989

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