Implementation of a full-envelope controller for a high-performance aircraft-Reference-Cited by-同舟云学术

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Implementation of a full-envelope controller for a high-performance aircraft

Published:1994-05 Issue:3 Volume:17 Page:578-583
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Adams Richard J.¹,Buffington James M.¹,Banda Siva S.¹

Affiliation:

1. Wright Laboratory WL/FIGC, Wright-Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.21236

Reference7 articles.

1. A fixed H∞ controller for a supermaneuverable fighter performing the herbst maneuver

2. Quadratic weights for asymptotic regulator properties

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Longitudinal Integrated Linear Parameter Varying Control for Morphing Aircraft in Large Flight Envelope;AIAA Atmospheric Flight Mechanics Conference;2017-06-02

2. Design of FLC for high-angle-of-attack flight using adaptive evolutionary algorithm;KSME International Journal;2003-02

3. Robust sampled-data H∞-flight-controller design for high α stability-axis roll maneuver;Control Engineering Practice;2000-07

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