2020 27th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) 2020
DOI: 10.23919/icins43215.2020.9133842
|View full text |Cite
|
Sign up to set email alerts
|

Determining of Equilibrium Positions of CubeSat Nanosatellite under the Influence of Aerodynamic and Gravitational Moments

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...

Citation Types

0
2
0

Year Published

2023
2023
2023
2023

Publication Types

Select...
2

Relationship

0
2

Authors

Journals

citations
Cited by 2 publications
(2 citation statements)
references
References 7 publications
0
2
0
Order By: Relevance
“…It is small in size and lightweight, reducing the launch cost. The small satellite classification is shown in Table 1 [ 4,5]. A CubeSat is a kind of nanosatellite [5].…”
mentioning
confidence: 99%
See 1 more Smart Citation
“…It is small in size and lightweight, reducing the launch cost. The small satellite classification is shown in Table 1 [ 4,5]. A CubeSat is a kind of nanosatellite [5].…”
mentioning
confidence: 99%
“…The small satellite classification is shown in Table 1 [ 4,5]. A CubeSat is a kind of nanosatellite [5]. The nanosatellite is small in size and lightweight.…”
mentioning
confidence: 99%