In this paper a systematic approach for weight selection has been applied. A classical phase lead compensator is used as weight (precompensator) in H infinity loop shaping for design of pitch controller for air vehicle. Analysis has been confined only to bode plots. The analysis and results achieved indicate that H infinity loop shaping control theory is a viable tool for design and synthesis of attitude control of air vehicle.
Weight selection in H- infinity loop shaping using lead/lag compensators
2006
6 Seiten, 8 Quellen
Conference paper
English
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