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2018 Fiscal Year Final Research Report

Design integration for nonlinear control systems via invariant manifold theory and the development of computational platform

Research Project

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Project/Area Number 26289128
Research Category

Grant-in-Aid for Scientific Research (B)

Allocation TypePartial Multi-year Fund
Section一般
Research Field Control engineering/System engineering
Research InstitutionNanzan University (2015-2018)
Nagoya University (2014)

Principal Investigator

Sakamoto Noboru  南山大学, 理工学部, 教授 (00283416)

Project Period (FY) 2014-04-01 – 2019-03-31
Keywords非線形制御 / 最適制御 / 計算プラットフォーム
Outline of Final Research Achievements

Throughout this research project, an approach has been taken such that concrete applications rather than abstract theories are investigated. Those examples include servo control design for lock-up clutch for automatic transmissions, optimal control for control moment gyros, stability augmentation for unmanned VTOL aircraft, gimbals control for a small-size rocket, swing up and stabilization for inverted pendulum, swing up and stabilization for flexible inverted pendulum, and swing up and stabilization for the Acrobot. Some of these experiments include the results that had never been reported. The success of these experimental results shows that the development of computational platform has been effectively achieved.

Free Research Field

制御理論

Academic Significance and Societal Importance of the Research Achievements

倒立振子振上げ実験,柔軟倒立振子振上げ実験,およびアクロボット振上げ実験は,これまで非線形制御では不可能だった制御性能が達成された.これは,本研究の学術的意義の高さを示していると言える.また,このような性能が可能となった背景には,計算プラットフォーム開発が十分に行われたことがある.このような計算プラットフォームを社会に還元することによって,基盤的工学の高度化が可能となるであろう.

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Published: 2020-03-30  

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