Design and Simulation of a Picosatellite Attitude Control Subsystem
碩士 === 國立成功大學 === 電機工程學系碩博士班 === 91 === PACE satellite is the first indigenous Picosat that attempts to achieve 3-axis stabilization. In this thesis, the design and simulation of the attitude control subsystem of the PACE satellite are presented. The requirement is to achieve 5 degree earth pointing...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2003
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/60817138147574330244 |