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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2000, Vol. 21 ›› Issue (3): 267-269.
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ZHANG Li-jun,XIAO Ying-yue,CHENG Peng
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Abstract:
This article designed a longitudinal flight/propulsion controller for flight control systems by using normalized left coprime factorization(normalized LCF) of robust theories and summarized some character and experience for the normalized LCF. The controller satisfied practical engineering requirements. The effect of the controller was good.
Key words: normalized left coprime fact or ization, r obust control, loop shaping
CLC Number:
V249
ZHANG Li-jun;XIAO Ying-yue;CHENG Peng. APPLICATION OF NORMALIZED LCF H∞ METHOE IN FLIGHT/PROPULSEON CONTROLLER DESIGN[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2000, 21(3): 267-269.
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https://hkxb.buaa.edu.cn/EN/Y2000/V21/I3/267