Determination of poles and zeros of transfer functions for flexible spacecraft attitude control†

DOI10.1080/00207177608932803zbMath0329.93017OpenAlexW2131564976MaRDI QIDQ4097151

Peter W. Likins, Yoshiaki Ohkami

Publication date: 1976

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207177608932803

Mathematics Subject Classification ID

Linear systems in control theory (93C05) Control/observation systems governed by ordinary differential equations (93C15) Software, source code, etc. for problems pertaining to systems and control theory (93-04) Model systems in control theory (93C99)

Related Items

Performance analysis of the segment alignment control system for the ten- meter telescope, Research on system zeros: a survey

Cites Work

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• A computational method for finding the zeros of a multivariable linear time invariant system
• Zeros determination in large-scale multivariable systems