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Development of kinematic GPS software, KINGS, and flight test evaluation
https://jaxa.repo.nii.ac.jp/records/40306
https://jaxa.repo.nii.ac.jp/records/4030673c552f9-64ab-4392-98c8-22ee48d5216e
名前 / ファイル | ライセンス | アクション |
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naltr0001357t.pdf (3.4 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Development of kinematic GPS software, KINGS, and flight test evaluation | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | キネマティックGPS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | KINGS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衛星航法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | GPS精密測位 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | GPSソフトウエア | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | オンザフライアルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 測位精度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 飛行試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アンビギティ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | kinematic GPS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | KINGS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | satellite navigation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | precise GPS positioning | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | GPS software | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | on the fly algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | positioning accuracy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flight test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ambiguity | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | キネマティックGPSソフトウエアKINGSの開発および飛行試験評価 | |||||
著者 |
辻井, 敏秋
× 辻井, 敏秋× 村田, 正秋× 張替, 正敏× 小野, 孝次× 稲垣, 敏治× Tsujii, Toshiaki× Murata, Masaaki× Harigae, Masatoshi× Ono, Takatsugu× Inagaki, Toshiharu |
|||||
著者所属 | ||||||
航空宇宙技術研究所 制御部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 企画室 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 制御部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 飛行実験部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 飛行実験部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Control Systems Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Planning Office | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Control Systems Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Flight Research Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Flight Research Division | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory 巻 1357T, p. 1-52, 発行日 1998-10 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | GPS搬送波位相干渉法による精密測位は、従来測地測量などの静止基線解析の分野で幅広く応用されているが、時々刻々と変化する基線に対しては適用が難しいとされてきた。ところが、近年、搬送波に内在する未知数(アンビギティ)を実時間で解くアルゴリズム(On-The-Fly(OTF)アルゴリズム)が多くの研究者によって開発され、移動体に対する精密測位も可能となってきた。本報告では、航技研で独自に開発した新しいOTFアルゴリズムを提案し、様々な実験による実証例を示す。GPS搬送波を用いた移動体の精密測位は、キネマティックGPS(KGPS)と呼ばれるが、航空技術研究所では独自のOTFアルゴリズムを核とするKGPSソフトウェア、KINGSを開発し、その性能評価を研究用航空機ドルニエ228を用いて行った。その結果、基線長20km以内、可視衛星5衛星以内の場合に、98%以上の確率でほぼ瞬時にアンビギティを解くことができた。アンビギティが正しく解けた場合の測位精度は約10cm(3σ)である。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Precise positioning using GPS carrier phase measurement has been widely used in static applications, i.e., geodetic surveying. However, it can also be applied to the precise positioning of a moving platform if an ambiguity contained in the GPS carrier phase measurement is resolved during the motion. The technique to resolve the ambiguity on the way/fly, which is called the OTF (On-The-Fly), has been investigated by many authors. In this paper, a new OTF algorithm is proposed and its feasibility for several kinds of applications is demonstrated. The differential GPS positioning using carrier phase measurements is called Kinematic GPS (KINGS). The Kinematic GPS Software, KINGS, in which the OTF is the most significant algorithm, was developed and its performance was evaluated by conducting a lot of flight experiments using a research aircraft of the National Aerospace Laboratory (NAL). As a result, the correct ambiguity was resolved nearly instantaneously with more than 98 percent probability when the distance between the aircraft receiver and the ground reference receiver was less than 20 km, and five or more satellites were observed. Once the ambiguity was resolved, the aircraft position was determined within 10 cm (3 sigma). | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001666000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1357T |