3333 An Open Source GPS Receiver for Small Satellite Applications

2005 ◽  
Vol 2005.5 (0) ◽  
pp. 393-394
Author(s):  
Takuji Ebinuma
2020 ◽  
Vol 2020 ◽  
pp. 1-12
Author(s):  
Pavel Kovar

The paper summarizes the experiences with the operation of the piNAV GPS receiver in a 1U unstabilized CubeSat operated on LEO orbit. piNAV L1 is a GPS receiver developed by an author for small satellite missions. The receiver is equipped with the 15 GPS L1 C/A channels and acquisition accelerator that shortens the cold start of the receiver on LEO to 65 s. The typical power consumption is 120 mW. Lucky-7 is a private 1U technological CubeSat with power budget 1 W that operates on the quasisynchronous polar orbit at altitude 520 km. One of its scientific missions is to test the operation of GPS. The space experiments proved the successful operation of the GPS receiver. The position information was available for approximately 80% of the time, where the position outage was caused by a satellite rotation and relatively long navigation signal reacquisition. The experimental data proved that the position availability can be improved by a higher-performance signal acquisition engine.


Energies ◽  
2020 ◽  
Vol 13 (16) ◽  
pp. 4097
Author(s):  
Vaclav Knap ◽  
Lars Kjeldgaard Vestergaard ◽  
Daniel-Ioan Stroe

CubeSats and small satellite solutions are increasing in popularity as they enable a fast, cheap, and agile way for satellite applications. An essential component of nearly every satellite is the energy storage device, which is practically equal to a battery. Consequently, an overview of past, present, and future battery technologies for CubeSats is presented. CubeSats use typically commercial off-the-shelf (COTS) batteries. They are not primarily dedicated to space, so their suitability to the space environment needs to be evaluated. Batteries are also considered as potentially dangerous goods. Thus, there are guidelines and standards that specify safety criteria and tests for the batteries in order to be allowed for transportation and launch. Furthermore, the character of satellites’ missions determines their demand on batteries in terms of current rates, depth-of-discharge, and lifetime. Thus, these expectations are discussed. A market survey was also carried out to identify currently available commercial battery solutions and their parameters. This work summarizes the status, requirements, and the market situation of batteries for CubeSats.


Author(s):  
Rachid Darbali-Zamora ◽  
Nicolas Cobo-Yepes ◽  
John E. Salazar-Duque ◽  
Eduardo I. Ortiz-Rivera ◽  
Amilcar A. Rincon-Charris

2006 ◽  
Vol 48 (5) ◽  
pp. 175-179 ◽  
Author(s):  
Naftali Herscovici ◽  
Christos Christodoulou ◽  
V. Lappas ◽  
G. Prassinos ◽  
A. Baker ◽  
...  

2018 ◽  
Vol 106 (3) ◽  
pp. 419-428 ◽  
Author(s):  
Keith B. Chin ◽  
Erik J. Brandon ◽  
Ratnakumar V. Bugga ◽  
Marshall C. Smart ◽  
Simon C. Jones ◽  
...  

2016 ◽  
Author(s):  
Robert Wright ◽  
Paul Lucey ◽  
Sarah Crites ◽  
Harold Garbeil ◽  
Mark Wood ◽  
...  

Sign in / Sign up

Export Citation Format

Share Document