並列タイトル等Stable Platform Evaluation Program and Stimulation Results
タイトル(掲載誌)航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-510
一般注記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.
資料番号: NALTR0510000
レポート番号: NAL TR-510
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44764&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ