Mixed Norm Control of a Helicopter-Reference-Cited by-同舟云学术

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Mixed Norm Control of a Helicopter

Published:2001-05 Issue:3 Volume:24 Page:555-565
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Trentini Michael¹,Pieper Jeff K.¹

Affiliation:

1. University of Calgary, Calgary, Alberta T2N 1N4, Canada

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/10.2514/2.4746

Reference26 articles.

1. AIAA Education Series;Padfield G. D.,1996

2. Linear quadratic optimal model-following control of a helicopter in hover

Cited by 8 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. Robust model predictive control for switched linear systems;ISA Transactions;2019-06

2. Survey on Flight Control Technology for Large-Scale Helicopter;International Journal of Aerospace Engineering;2017

3. Robust optimal attitude control of a laboratory helicopter without angular velocity feedback;Robotica;2014-02-28

4. Robust LQR Attitude Control of a 3-DOF Laboratory Helicopter for Aggressive Maneuvers;IEEE Transactions on Industrial Electronics;2013-10

5. Nonlinear adaptive model following control for a 3-DOF tandem-rotor model helicopter;Control Engineering Practice;2010-08

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