Published January 1, 2017
| Version v1
Conference paper
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Precise Astroinertial Attitude Determination of a Maneuvering Land-survey Satellite
- 1. Samara State Tech Univ, Dept Nav Guidance & Control, 244 Molodogvardeyskaya Str, Samara 443100, Russia
- 2. Istanbul Tech Univ, Aeronaut & Astronaut Fac, TR-34469 Istanbul, Turkey
Description
We consider some principal problems on precise attitude determination of the maneuvering land-survey satellites placed on the orbit altitudes from 600 up to 1000 km. We present onboard discrete algorithms for signal processing, calibration and alignment of astroinertial attitude determination system which is a part of the strapdown inertial navigation system.
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