Abstract
Optical remote sensing satellites are generally composed of two parts which are satellite platform and camera. In order to evaluate the satellites on-orbit working status, it is necessary to carry out micro-vibration tests on the ground to simulate the satellite's on-orbit working status. This paper proposes a micro-vibration test method based on dual-stage gravity compensation system. The gravity compensation both on satellite platform and camera can be achieve separately by using the dual-stage system, and evaluates the effectiveness of satellite micro-vibration suppression measures. This method adopts top suspension and bottom elastic support to achieve dual-stage gravity compensation, and the specification of suspension frequency is lower than 1 Hz and the support frequency is lower than 2.5 Hz. The method proposed has been successfully applied to the micro-vibration test of a flight model satellite.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Laskin RA, Sirlin SW (1986) Future payload isolation and pointing system technology. J Guidance 9(4):469–477
Bialke B (1997) A compilation of reaction wheel induced spacecraft disturbances. In: Proceedings of the 20th annual AAS guidance and control conference, pp 97–119
Rui X, Zhang J, Wang X, Rong B, He B, ** Z (2022) Multibody system transfer matrix method: the past, the present, and the future. Int J Mech Syst Dyn 2(1):3–26
Liu MH, Liu C, **ang SH, Han XJ (2022) Effect of simulated boundary on dynamic characteristics of satellite. Space Environ Eng 39(3):225–229
Gao HY, Wang D, Li D et al (2019) Simulation and experimental verification of dynamic characteristics of spacecraft micro-vibration test fixture. Spacecraft Environ Eng 36(3):252–256
Spacecraft Micro-Vibration Test Method. QJ 20893, (2018)
Liu MH, Wang J, Jiao AC et al (2014) A method for simulating the free boundary condition of satellite on orbit. Spacecraft Environ Eng 31(1):19–24
Cornelius D, Oscar S, Alvarez-Salazar (2018) Spacecraft micro-vibration: a survey of problems, experiences, potential solutions, and some lessons learned. NASA/TM-2018-220075
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2024 The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Zhu, J., Zhang, W., Liu, C., Qiu, H., Lu, D. (2024). A Micro-vibration Test Method for Satellite Based on Dual-Stage Gravity Compensation System. In: Rui, X., Liu, C. (eds) Proceedings of the 2nd International Conference on Mechanical System Dynamics. ICMSD 2023. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-99-8048-2_266
Download citation
DOI: https://doi.org/10.1007/978-981-99-8048-2_266
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-99-8047-5
Online ISBN: 978-981-99-8048-2
eBook Packages: EngineeringEngineering (R0)