DocumentCode :
3642562
Title :
Mission analysis and planning of a CANSAT
Author :
Cihan Çabuloğlu;Hüseyin Aykiş;Resul Yapacak;Erhan Çalişkan;Ömer Ağirbaş;Şaban Abur;Süleyman Soyer;Halit Türkmen;Serdar Ay;Yasin Karataş;Emre Aydemır;Mansur &
Author_Institution :
Turkish Air Force Academy, Istanbul, TURKEY
fYear :
2011
fDate :
6/1/2011 12:00:00 AM
Firstpage :
794
Lastpage :
799
Abstract :
In this study, a mini model satellite that measures pressure, the temperature and its location. The Project is called as “cansat”. It is the combined name of the “can” and “satellite” words. Can-sized and can-shaped CANSAT - it is new trend in Turkey - this is the first step to reach the space and its technology. This micro-satellite will have lots of capabilities after adding electronic equipments, sensors and GPS. CANSAT is provided to take a certain altitude by an R/C aircraft. Then it is allowed to free fall from the R/C aircraft and it can land on ground with the help of a parachute which we produce. The mission objectives are; temperature, pressure, altitude and humidity measurement, landing to the desired point. Also after measuring these data, they will be sent them to the central database. These capabilities are provided with the sensors and GPS which they´re readymade. These sensors will mount to electronic signal precisely and also GPS receiver will mount the same signal. The radio receiver will install to RF module to have connection with the micro-satellite. CANSAT project is a chance to use theoretical knowledge in practice for students.
Keywords :
"Global Positioning System","Payloads","Atmospheric modeling","Protocols","Application specific integrated circuits"
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies (RAST), 2011 5th International Conference on
Print_ISBN :
978-1-4244-9617-4
Type :
conf
DOI :
10.1109/RAST.2011.5966951
Filename :
5966951
Link To Document :
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