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...
Saved in:
Main Authors: | Dario Modenini, Giacomo Curzi, Paolo Tortora |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2018-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2018/3582508 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Thermal modeling and empirical verification of multi unit small satellites
by: Anwar Ali, et al.
Published: (2025-03-01) -
Thermal Design and Verification of Spherical Scientific Satellite Q-SAT
by: Yunhan He, et al.
Published: (2021-01-01) -
Automatic Task Planning and Its On-Orbit Verification of Agile Remote Sensing Satellite
by: Zhang Yahang, et al.
Published: (2023-01-01) -
Spatio-temporal evolution and driving forces of urban gravity centers and ecological security risk gravity centers in China
by: Peng Chen, et al.
Published: (2025-01-01) -
Design and Verification of Large-Diameter Tower Sharding Platform for Wind Turbine
by: Jiawen LAN, et al.
Published: (2025-01-01)