제어로봇시스템학회:학술대회논문집
- 1995.10a
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- Pages.368-371
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- 1995
Dynamics and control of a large spacecraft with flexible appendages in gravitational field
- Nohmi, Masahiro (Dep. of Aero. and Space Eng., Tohoku Univ.) ;
- Uchiyama, Masaru (Dep. of Aero. and Space Eng., Tohoku Univ.)
- Published : 1995.10.01
Abstract
This paper describes dynamic analysis and attitude control of a large spacecraft with flexible appendages in gravitational field. The effect of attitude control and vibration control of flexible appendages in gravitational field has been clarified. We demonstrate some simulations in gravitational field for some cases, and suggest the effects of gravitational torque, parameters of flexible appendages, attitude control and vibration control of flexible appendages.