The design techniques presented are applicable to satellite missions where the dominant environmental torques are well understood and lend themselves to accurate analytical modeling. The techniques were applied to the Particles and Fields subsatellites of the Apollo 15 and 16 spacecraft and the flight results show good agreement with the attitude determination estimates obtained.
Exploiting environmental torques for attitude control and determination of spin stabilized satellites
Das Ausnutzen der Umgebungsdrehmomente fuer die Hoehenregelung und Drallbestimmung stabilisierter Satelliten
Israel Journal of Technology ; 12 , 3-4 ; 151-159
1974
, 12 Quellen
Article (Journal)
English
Torques and attitude sensing in spin-stabilized synchronous satellites
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