不確かさを有するスケジューリングパラメータを用いたゲインスケジュールド飛行制御器の MuPAL-αに対する設計と性能検証

• 資料種別: 記事
• タイトル: 不確かさを有するスケジューリングパラメータを用いたゲインスケジュールド飛行制御器の MuPAL-αに対する設計と性能検証
• 著者・編者: 佐藤 昌之
• 著者標目: 佐藤 昌之
• 並列タイトル等: Design and Performance Check of Gain-Scheduled Flight Controller Depending on Uncertain Scheduling Parameters for MuPAL-α
• タイトル（掲載誌）: 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
• 巻号年月日等（掲載誌）: 68(1):2020.2
• 掲載巻: 68
• 掲載号: 1
• 掲載ページ: 12-23
• 掲載年月日（W3CDTF）: 2020-02
• ISSN（掲載誌）: 1344-6460
• ISSN-L（掲載誌）: 1344-6460
• 出版事項（掲載誌）: 東京 : 日本航空宇宙学会
• 出版地（国名コード）: JP
• 本文の言語コード: jpn
• 件名標目: Gain-scheduled Flight Controller; Uncertain Scheduling Parameter; Flight Test
• NDLC: ZN25
• 対象利用者: 一般
• 所蔵機関: 国立国会図書館
• 請求記号: Z74-B503
• 連携機関・データベース: 国立国会図書館 : 国立国会図書館雑誌記事索引; https://ndlsearch.ndl.go.jp
• 書誌ID（NDLBibID）: 030253682; http://id.ndl.go.jp/bib/030253682
• 整理区分コード: 632

• 要約等: <p>This paper addresses the design problem of Gain-Scheduled (GS) flight controllers, in which only inexact scheduling parameters are available, for aicraft motion control. Most of existing design methods for GS controllers implicitly suppose that exact scheduling parameters are available. However, this does not always hold true in practice, which has invoked the research on the design of GS controllers depending on inexact scheduling parameters. We design a GS flight controller for the lateral-directional motion of JAXA's fixed-wing experimental aircraft MuPAL-α using a recently proposed design method which guarantees the pre-defined control performance under the bounded uncertainties in the provided scheduling parameters. We examine the applicability and performance of our controller by flight tests. </p>
• DOI: 10.2322/jjsass.68.12
• オンライン閲覧公開範囲: インターネット公開
• 連携機関・データベース: 科学技術振興機構 : J-STAGE; http://www.jstage.jst.go.jp

• 要約等: <p>This paper addresses the design problem of Gain-Scheduled (GS) flight controllers, in which only inexact scheduling parameters are available, for aicraft motion control. Most of existing design methods for GS controllers implicitly suppose that exact scheduling parameters are available. However, this does not always hold true in practice, which has invoked the research on the design of GS controllers depending on inexact scheduling parameters. We design a GS flight controller for the lateral-directional motion of JAXA's fixed-wing experimental aircraft MuPAL-α using a recently proposed design method which guarantees the pre-defined control performance under the bounded uncertainties in the provided scheduling parameters. We examine the applicability and performance of our controller by flight tests. </p>
• DOI: 10.2322/jjsass.68.12; https://doi.org/10.2322/jjsass.68.12
• 関連情報（URI）: http://id.ndl.go.jp/bib/030253682; https://ndlsearch.ndl.go.jp/books/R000000004-I030253682; https://www.jstage.jst.go.jp/article/jjsass/68/1/68_68_12/_pdf
• 参照: A New Method for Gain-Scheduled Output Feedback Controller Design Using Inexact Scheduling Parameters; https://cir.nii.ac.jp/crid/1362825893410847104; Control of Linear Parameter Varying Systems with Applications; https://cir.nii.ac.jp/crid/1363388844803003776; Robust Control and Linear Parameter Varying Approaches; https://cir.nii.ac.jp/crid/1363670320957835648
• 連携機関・データベース: 国立情報学研究所 : CiNii Research; https://cir.nii.ac.jp/
• 提供元機関・データベース: Japan Link Center; https://japanlinkcenter.org/top; 雑誌記事索引データベース; https://ndlsearch.ndl.go.jp; Crossref; https://www.crossref.org; CiNii Articles
• 書誌ID（NDLBibID）: 030253682; http://id.ndl.go.jp/bib/030253682
• NII論文ID: 130007795332