Print Email Facebook Twitter Accuracy of attitude control systems for satellites using double gimballed momentum wheels Title Accuracy of attitude control systems for satellites using double gimballed momentum wheels Author Boersma, G. Sonnenschein, F.J. Institution National Aerospace Laboratory NLR Date 1973-05-17 Subject Satellite attitude controldouble gimballed momentum wheelspointing accuracycontrol lawssemi active controlestimation techniques To reference this document use: http://resolver.tudelft.nl/uuid:1c0e9746-35b5-4168-84a4-4b20ff61fd39 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 73055 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1973 National Aerospace Laboratory NLR Files PDF NLR_TR_73055_U.pdf 40.74 MB Close viewer /islandora/object/uuid:1c0e9746-35b5-4168-84a4-4b20ff61fd39/datastream/OBJ/view