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http://dx.doi.org/10.5139/JKSAS.2016.44.1.57

Comparison Study of H-infinity Controller Design Algorithms for Spacecraft Attitude Control  

Rhee, Seung-Wu (Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.44, no.1, 2016 , pp. 57-69 More about this Journal
Abstract
There are three kinds of algorithms(2-ARE, mu-synthesis, LMI) for controller design using closed-loop shaping method. This paper provides the summary of background theory of three algorithms and $H_{\infty}$ controller design results for spacecraft attitude control using the three controller design tools of Matlab$^{TM}$ Toolbox for comparison. As a result, it reveals that LMI design method is more reliable as well as easier than others for spacecraft attitude control design. Comparison results are as follow: 2-ARE method and LMI method provide almost same results in robust stability, robust performance and control authority level. But 2-ARE method is more sensitive than LMI method with respect to proper design of weighting functions: 2-ARE method is more difficult than LMI method in weighting function design. The design result of mu-synthesis method shows worse performance and requires bigger control authority than others.
Keywords
$H_{\infty}$ Controller; 2-ARE; mu-Synthesis; LMI; Robust Stability; Robust Performance; Spacecraft Attitude Control;
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Times Cited By KSCI : 2  (Citation Analysis)
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