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...
Saved in:
Main Authors: | , , |
---|---|
Other Authors: | |
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 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |