Controls design challenge - A variable structure approach

Author:

Thukral Ajay1,Innocenti Mario1

Affiliation:

1. Auburn University, Auburn, Alabama 36849

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

Reference19 articles.

Cited by 7 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. Nonlinear H∞ robust control applied to F-16 aircraft with mass uncertainty using control surface inverse algorithm;Journal of the Franklin Institute;2008-11

2. Apache Helicopter Stabilization Using Neural Dynamic Programming;Journal of Guidance, Control, and Dynamics;2002-01

3. Neuro-dynamic programming applied to helicopter flight control;18th Applied Aerodynamics Conference;2000-08-14

4. Nonlinear H 8 Flight Control of General Six-Degree-of-Freedom Motions;Journal of Guidance, Control, and Dynamics;2000-03

5. Flight control reconfiguration on sliding modes;Guidance, Navigation, and Control Conference;1997-08-11

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