Abstract The possibility of identification of motion parameters of a low-orbit spacecraft using readings of a three-axis magnetometer and solar position sensor, without integration of the Euler’s dynamic equations or direct measurement of the object’s angular velocity, is considered.
An alternative algorithm for the spacecraft information system with magnetometer and solar sensor
Cosmic Research ; 47 , 4 ; 330-336
2009-08-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
An alternative algorithm for the spacecraft information system with magnetometer and solar sensor
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