@techreport{oai:jaxa.repo.nii.ac.jp:00044764,
 author = {新田, 慶治 and 大坪, 孔治 and 小口, 美津夫 and NITTA, Keiji and OTSUBO, Koji and OGUCHI, Mitsuo},
 month = {Aug},
 note = {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},
 title = {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},
 year = {1977}
}