Please use this identifier to cite or link to this item: http://hdl.handle.net/2248/6742
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dc.contributor.authorNirmal, K-
dc.contributor.authorSreejith, A. G-
dc.contributor.authorMathew, J-
dc.contributor.authorMayuresh, Sarpotdar-
dc.contributor.authorAmbily, S||Prakash, A-
dc.contributor.authorSafonova, M-
dc.contributor.authorMurthy, J-
dc.date.accessioned2020-11-10T02:34:52Z-
dc.date.available2020-11-10T02:34:52Z-
dc.date.issued2016-12-
dc.identifier.citationJournal of Astronomical Telescopes, Instruments, and Systems, Vol. 2, No. 4, pp. 047001-1- 047001-9en_US
dc.identifier.issn2329-4221-
dc.identifier.urihttp://prints.iiap.res.in/handle/2248/6742-
dc.descriptionRestricted Access http://dx.doi.org/10.1117/1.JATIS.2.4.047001 © SPIE--The International Society for Optical Engineeringen_US
dc.description.abstractWe describe the development and implementation of a light-weight, fully autonomous 2-axis pointing and stabilization system designed for balloon-borne astronomical payloads. The system is developed using offthe-shelf components such as Arduino Uno controller, HMC 5883L magnetometer, MPU-9150 inertial measurement unit, and iWave GPS receiver unit. It is a compact and rugged system which can also be used to take images/video in a moving vehicle or in real photography. The system performance is evaluated from the ground, as well as in conditions simulated to imitate the actual flight by using a tethered launch.en_US
dc.language.isoenen_US
dc.publisherSPIE-The International Society for Optical Engineeringen_US
dc.subjectBalloon experimenten_US
dc.subjectAttitude sensoren_US
dc.titlePointing system for the balloon-borne astronomical payloadsen_US
dc.typeArticleen_US
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