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초록
Flight Dynamics and Control Laboratory at Inha University has developed a single axis rate table successfully, and is expanding the work to 3-axis system. The mximum speed will be 2 rev./sec for roll axis and 1 rev./sec for yaw axis.
- 제목
- Development of a Medium Size 3-Axis Rate Table
- 저자
- PARK CHOONBAE
- 학회명
- Proceedings of JSASS 15th International Sessions in 39th Aircarft Symposium