Analysis of the Perpendicularity Influence of the Gyrowheel Support on the Spacecraft Angular Velocity Measurement Accuracy

Author:

Xiaokun Liu,Jian Zhang,Jun Fu,Dongqing Gu,Bin Song

Publisher

Springer Singapore

Reference7 articles.

1. Liang, L.I., Wang, H., Liu, L.Y.: Development of micro-satellite constellation and formation technologies. Space Electron. Technol. 1, 1–14 (2017)

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3. Cain, J.S.: Investigation of the crossed flexure pivot and the dynamics of the momentum management system spacecraft control component and the dynamically tuned gyroscope. Carleton University, Ottawa (1999)

4. Ren, Y., Chen, X., Cai, Y.: Attitude rate measurement and control integration using magnetically suspended control and sensitive gyroscopes. IEEE Trans. Ind. Electron. 65, 4921–4932 (2018)

5. Tyc, G., Staley, D.A., Whitehead, W.R.: GyroWheel$$^{TM}$$-an innovative new actuator/sensor for 3-axis spacecraft attitude control. In: 13th Annual AIAA/USU Conference on Small Satellites, pp. 1–13. AIAA, Toronto(1999)

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