Title of article
A balloon trajectory prediction system Original Research Article
Author/Authors
I. Musso، نويسنده , , Joé A. Cardillo، نويسنده , , O. Cosentino، نويسنده , , A. Memmo، نويسنده ,
Issue Information
دوهفته نامه با شماره پیاپی سال 2004
Pages
5
From page
1722
To page
1726
Abstract
Safety requirements and the increase in balloon flight duration make a computerized balloon control system essential. Starting with a global thermodynamic model of a stratospheric balloon (NASA-SINBAD) and 48-h wind forecast data, a flexible system can be built to predict its trajectory. In order to increase the trajectory forecast accuracy, the thermodynamic model of SINBAD, related to infrared radiation and albedo, has been improved. The model and the methodology have been evaluated by comparing the altitude excursion of some already flown zero-pressure balloons, with the altitude excursion computed by SINBAD; meteorological and satellite data (METEOSAT) and meteorological forecast data have been used as input. This system, connected during the mission to the balloonʹs managing unit, will continuously update the forecast trajectory and will enable real and simulated data to be compared. In this way it will also be possible to simulate the balloon flight trajectory in case of any failures. This paper explains the solution adopted for this system and the application that was carried out for the Italian Space Agencyʹs 2002 summer balloon campaign.
Keywords
Scientific ballooning , Balloon trajectory prediction
Journal title
Advances in Space Research
Serial Year
2004
Journal title
Advances in Space Research
Record number
1129454
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