Abstract
Aryabhata was a spin-stabilised satellite. Attitude determination was required for the evaluation of the stabilisation system and for scientific experiments. Temperature sensors were required for the performance evaluation of the onboard systems and of the thermal control system. A detailed description of the sensors used for these functions inAryabhata is given.
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Albus J S 1961 Digital Solar Aspect Sensor NASA TN-D-1062
Bartey W C, McCracken K G and Rao U R 1967IEEE Tran. Aerosp. Electron. AES-3 No. 2 230
Kalweit C C 1969 ESRO I Attitude measurement system ESRO TN-99 (ESTEC)
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Kasiviswanathan, G.A., Varadarajulu, V.P.V., Venkateswaran, P.R. et al. Attitude and temperature sensors. Proc. Indian Acad. Sci. (Engg. Sci.) 1, 173–184 (1978). https://doi.org/10.1007/BF02843542
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DOI: https://doi.org/10.1007/BF02843542