scholarly journals Conceptual Optical Design of a Synthetic Aperture Telescope by Small Satellite Formation Flying for GEO Remote Sensing

2020 ◽  
Vol 18 (3) ◽  
pp. 101-107
Author(s):  
Norihide MIYAMURA ◽  
Ryo SUZUMOTO ◽  
Satoshi IKARI ◽  
Shinichi NAKASUKA
Keyword(s):  
Remote Sensing ◽  
Formation Flying ◽  
Optical Design ◽  
Synthetic Aperture ◽  
Small Satellite ◽  
Satellite Formation Flying ◽  
Satellite Formation

Communication experiments for autonomous small satellite formation flying operation - Application for release and capture

2001 ◽  
Author(s):  
Yasuhiro Takeshita ◽  
Isao Kudo ◽  
Yoshitsugu Toda ◽  
Tokanori Adachi ◽  
Hiroshi Murakami ◽  
...  
Keyword(s):  
Formation Flying ◽  
Small Satellite ◽  
Satellite Formation Flying ◽  
Satellite Formation

A Review of Impending Small Satellite Formation Flying Missions

2015 ◽  
Author(s):  
Saptarshi Bandyopadhyay ◽  
Giri P. Subramanian ◽  
Rebecca Foust ◽  
Daniel Morgan ◽  
Soon-Jo Chung ◽  
...  
Keyword(s):  
Formation Flying ◽  
Small Satellite ◽  
Satellite Formation Flying ◽  
Satellite Formation

scholarly journals The Trend and Prospect of Small Satellite Formation Flying Technology

2003 ◽  
Vol 31 (7) ◽  
pp. 136-149 ◽  
Author(s):  
Yeong-Geun Jang ◽  
Mun-Sik Park ◽  
Seong-Mun Yu ◽  
Sang-Yeong Park ◽  
Gyu-Hong Choe
Keyword(s):  
Formation Flying ◽  
Small Satellite ◽  
Satellite Formation Flying ◽  
Satellite Formation

Making aerosol measurements using small satellite formation flying

2013 ◽  
Vol 51 (5) ◽  
pp. 396-399
Author(s):  
A. Sh. Mekhtiev ◽  
Kh. G. Asadov ◽  
K. Kh. Ismailov
Keyword(s):  
Formation Flying ◽  
Small Satellite ◽  
Satellite Formation Flying ◽  
Satellite Formation

Fault Tolerant Guidance of Under-Actuated Satellite Formation Flying Using Inter-Vehicle Coulomb Force

2019 ◽  
Vol 2 (1) ◽  
pp. 43-52
Author(s):  
Alireza Alikhani ◽  
Safa Dehghan M ◽  
Iman Shafieenejad
Keyword(s):  
Fault Tolerance ◽  
Formation Flying ◽  
Fault Tolerant ◽  
Coulomb Force ◽  
Control Law ◽  
Triangular Form ◽  
Satellite Formation Flying ◽  
Satellite Formation ◽  
Guidance Law ◽  
Tolerance Approach

In this study, satellite formation flying guidance in the presence of under actuation using inter-vehicle Coulomb force is investigated. The Coulomb forces are used to stabilize the formation flying mission. For this purpose, the charge of satellites is determined to create appropriate attraction and repulsion and also, to maintain the distance between satellites. Static Coulomb formation of satellites equations including three satellites in triangular form was developed. Furthermore, the charge value of the Coulomb propulsion system required for such formation was obtained. Considering Under actuation of one of the formation satellites, the fault-tolerance approach is proposed for achieving mission goals. Following this approach, in the first step fault-tolerant guidance law is designed. Accordingly, the obtained results show stationary formation. In the next step, tomaintain the formation shape and dimension, a fault-tolerant control law is designed.

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