ロボティクス・メカトロニクス講演会講演概要集
Online ISSN : 2424-3124
セッションID: 2P1-L06
会議情報

空力モデルに基づくドローンの飛行特性推定
*福田 一浩取田 礼譲岸 拓志得竹 浩砂田 茂田辺 安忠米沢 宏一
著者情報
キーワード: UAV, Aerodynamics, Gust responce
会議録・要旨集 フリー

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抄録

Robust flight control under adverse environments is required. As an existing method, several systematic control system design methods including H control have been established. However, as a disadvantage of these methods, control performance may become remarkably conservative, especially when large uncertainty exists. As an element of large uncertainty, modeling error of target dynamics can be mentioned. By calibrating this modeling error, maintainability can be avoided and control performance can be expected to improve. The final objective is to design a controller that can estimate modeling errors in real time and provide adaptive control inputs. As the first step in this paper, we designed an observer that can estimate uncertainty in real time from motion history for modeling error calibration.

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© 2018 一般社団法人 日本機械学会
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