TY - GEN
T1 - Meteorological balloons as an experimental platform for scientific and engineering research
AU - Chen, Alfred B.
AU - Chiu, Cheng Hsiu
AU - Wen, Shao Chun
AU - Lai, Hsuan Chen
AU - Su, Han Tzong
AU - Hsu, Rue Ron
PY - 2013
Y1 - 2013
N2 - The exploration by the in-situ measurement in the stratosphere, approximately 8-50 km height, can be done by sounding balloons exclusively. The scientific sounding balloon was used in the past decades to carry up to tones of the scientific instruments to the upper atmosphere and reached a great contribution in the atmosphere science, space science, and astrophysics. But the large scientific balloon can be launched in the limited sites for the safety reason and its cost is not affordable by all scientists. By integrating the miniaturized sensors, processor board and meteorological sounding balloon, we developed an experimental platform to carry small instruments up to 33 km altitude and transmit data to mobile ground stations. This experimental platform has the advantages of lightweight, inexpensive, disposable, and safe. It is not only can be employed in the scientific measurement but also able to act as a testbed for the new technologies which is going to be used in sounding rocket or satellite missions. The system structure of this platform and a successful flight experiment are introduced in this paper, and the new possible improvement is also discussed.
AB - The exploration by the in-situ measurement in the stratosphere, approximately 8-50 km height, can be done by sounding balloons exclusively. The scientific sounding balloon was used in the past decades to carry up to tones of the scientific instruments to the upper atmosphere and reached a great contribution in the atmosphere science, space science, and astrophysics. But the large scientific balloon can be launched in the limited sites for the safety reason and its cost is not affordable by all scientists. By integrating the miniaturized sensors, processor board and meteorological sounding balloon, we developed an experimental platform to carry small instruments up to 33 km altitude and transmit data to mobile ground stations. This experimental platform has the advantages of lightweight, inexpensive, disposable, and safe. It is not only can be employed in the scientific measurement but also able to act as a testbed for the new technologies which is going to be used in sounding rocket or satellite missions. The system structure of this platform and a successful flight experiment are introduced in this paper, and the new possible improvement is also discussed.
UR - http://www.scopus.com/inward/record.url?scp=84897705015&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84897705015&partnerID=8YFLogxK
U2 - 10.1109/CACS.2013.6734103
DO - 10.1109/CACS.2013.6734103
M3 - Conference contribution
AN - SCOPUS:84897705015
SN - 9781479923847
T3 - 2013 CACS International Automatic Control Conference, CACS 2013 - Conference Digest
SP - 36
EP - 40
BT - 2013 CACS International Automatic Control Conference, CACS 2013 - Conference Digest
T2 - 2013 CACS International Automatic Control Conference, CACS 2013
Y2 - 2 December 2013 through 4 December 2013
ER -