Abstract
This paper presents the simulation studies of the dynamics of short tethered satellite system during the deployment phase. The deployment dynamics of the tethered system is dominated by the tether oscillations and the three-dimensional attitude dynamics of the sub-satellite. The dynamic characters of the system are investigated, and probable control strategies that can be adopted for the faithful and hassle-free deployment of the tether are discussed. Tether is proposed to be released with an initial velocity with constant deceleration using tension in tether. Dynamics of a short tether of 10 m length connected to a 10 kg 3U sub-satellite is considered in the study. Deployment with tether in tension and without tension in tether is discussed.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Dubanchet V, Saussié D, Alazard D, Bérard C, Le Peuvedic C (2014) Modeling and control of a space robot for active debris removal. In: ESA GNC 2014 9th international ESA conference on guidance, navigation and control systems, Porto, Portugal 2–6 June 2014
Aslanov VS, Ledkov AS (2012) Dynamics of tethered satellite systems. Woodhead Publishing Limited, UK
Beletsky VV, Levin EM Dynamics of space tether systems, vol 83. Advances in the Astronautical Sciences, California
Liu Y, Zhou J (2016) Attitude dynamics and thrust control for short tethered sub-satellite in deployment. In: Proc IMechE Part G: J Aerosp Eng
Huang P, Zhang F et al (2016) Coordinated coupling control of tethered space robot using releasing characteristics of space tether. Adv Space Res Sci Direct
Yu BS, Wen H, Jin DP (2018) Review of deployment technology for tethered satellite systems. Acta Mech Sin 34(4):754–768. https://doi.org/10.1007/s10409-018-0752-5
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Sangeetha, G.R., Ganesan, H. (2020). Simulation of the Dynamics and Control of Tethered Small Satellite Deployment. In: Sastry, P.S., CV, J., Raghavamurthy, D., Rao, S.S. (eds) Advances in Small Satellite Technologies. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-1724-2_4
Download citation
DOI: https://doi.org/10.1007/978-981-15-1724-2_4
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-1723-5
Online ISBN: 978-981-15-1724-2
eBook Packages: EngineeringEngineering (R0)