WEKO3
アイテム
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ステーブル・プラットホーム動作評価プログラムとシミュレーション結果について
https://jaxa.repo.nii.ac.jp/records/44764
https://jaxa.repo.nii.ac.jp/records/44764cc84183c-c605-4e4f-bae2-ed2c8f24aafd
名前 / ファイル | ライセンス | アクション |
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naltr00510.pdf (3.7 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ステーブル・プラットホーム動作評価プログラムとシミュレーション結果について | |||||
言語 | ||||||
言語 | jpn | |||||
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(英) | ||||||
その他のタイトル | Stable Platform Evaluation Program and Stimulation Results | |||||
著者 |
新田, 慶治
× 新田, 慶治× 大坪, 孔治× 小口, 美津夫× NITTA, Keiji× OTSUBO, Koji× OGUCHI, Mitsuo |
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著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属 | ||||||
航空宇宙技術研究所宇宙研究グループ | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Space Technology Research Group, National Aerospace Laboratory(NAL) | ||||||
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 TR-510 巻 510, p. 128, 発行日 1977-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The stable platform behavior evaluation program was developed during a special study regarding the Ineritial Guidance System. Gyro and accelerometer mathematical models, 4-gimbal cluster mathematical models, gimbal drive servomotor mathematical models and lead and lag phase network mathematical models were formulated, with platform system synthesis conducted to determine the numerical value of platform servo-parameters related to stability and torque stiffness. The platform behavior Evolution program was then derived in conjunction with the formulated mathematical models mentioned above and the predetermine numerical value of the servo-parameters. Computer test runs of the program for the ETS-1 mission trajectory showed the program to be fully applicable with high accuracy to platform behavior performance simulation, and to be very useful in synthesizing platform servosystem parameters prior to development of new hardware. | |||||
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: NALTR0510000 | |||||
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-510 |