An optimization method for nano-satellite and pico-satellite separation through a two mass-one spring system

This paper studies the picosatellite ejection system from a nanosatellite, using one spring two mass ejection model. It is desired that both satellites maintain a long communication time after separation though they do not carry propulsion system. Moreover, the picosatellite is required to return to...

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Bibliographic Details
Main Authors: Lau, Zirui, Low, Kay Soon, Goh, Shu Ting
Other Authors: School of Electrical and Electronic Engineering
Format: Conference or Workshop Item
Language:English
Published: 2014
Subjects:
Online Access:https://hdl.handle.net/10356/79574
http://hdl.handle.net/10220/24138
http://www.researchgate.net/publication/260821673_An_Optimization_Method_for_Nano-satellite_and_Pico-satellite_Separation_through_a_Two_Mass-One_Spring_System
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Institution: Nanyang Technological University
Language: English