Experimental Verification of a Simple Method for Accurate Center of Gravity Determination of Small Satellite Platforms
We propose a simple and relatively inexpensive method for determining the center of gravity (CoG) of a small spacecraft. This method, which can be ascribed to the class of suspension techniques, is based on dual-axis inclinometer readings. By performing two consecutive suspensions from two different...
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Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Wiley
2018-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2018/3582508 |
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