OCHI Yoshimasa

ID:9000248243501

Department of Aerospace Engineering, National Defense Academy (2010年 CiNii収録論文より)

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  • I-PD Flight Controller Design based on Integral-Type Optimal Servomechanism

    KONDO Hiroyuki , OCHI Yoshimasa

    This paper describes a design method of an I-PD (integral preceded by proportional-derivative) controller for a single-input-single-output plant. The proposed method, which is relatively simple compar …

    SICE Journal of Control, Measurement, and System Integration 3(6), 448-455, 2010-11-30

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