Micro-Satellite Configuration of Discoid and Asymmetrical, Gyroless with Thrusters Three-Axis Robust Control and Stability Analysis
The center of mass of the micro-satellite can offset due to fuel consumption in the course of propulsion, with the interference of external orbital environment such as gravity gradient torque and solar radiation torque. If the structural shape is discoid and asymmetrical, the attitude control may be...
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| Format: | Article |
| Language: | English |
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Taiwan Association of Engineering and Technology Innovation
2014-01-01
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| Series: | International Journal of Engineering and Technology Innovation |
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| Online Access: | http://ojs.imeti.org/index.php/IJETI/article/view/125 |
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