Martti Hallikainen Aalto University / Jaan Praks Aalto University / Aalto University / Aarto Visala Aalto University / Finnish Meteorological Institute / SATELLITE DURING DE-ORBITING EXPERIMENT WITH PLASMA BRAKE Osama Khurshid Aalto University / /
IndustryTerm
satellite deceleration rate measurement data / satellite orbital plane / satellite / satellite inertia / inertia products / satellite angular momentum error vector / satellite-tether system / satellite mechanical model / collected satellite position / satellite inertia changes / satellite body / satellite mass distribution / de-orbiting device / satellite spinning / satellite inertia principal axes / /
Organization
Aarto Visala Aalto University / Multidisciplinary Institute of Digitalisation and Energy / Congress / CubeSat mission / JC2Sat-FF mission / Aalto University / Jaan Praks Aalto University / Aalto University’s School of Electrical Engineering / IAC-12-B4 / 2 / 11 / x15102 ATTITUDE DYNAMICS ANALYSIS OF AALTO-1 SATELLITE DURING DE-ORBITING EXPERIMENT WITH PLASMA BRAKE Osama Khurshid Aalto University / Finnish Meteorological Institute / International Astronautical Federation / Martti Hallikainen Aalto University / /
Person
Cal Poly / Anton de Ruiter / Matthias Buhl Berlin / /
Position
Prime Minister / fault-tolerant magnetic spin stabilizing controller / radiation monitor / spin controller / damping model for elastic materials / current satellite mechanical model / the princertain design restrictions and limitations / controller / /
Product
Satellite / /
PublishedMedium
European Journal of Physics / /
Technology
radiation / remote sensing / pekka.janhunen@fmi.fi Matthias Buhl Berlin Space Technologies / /
63rd International Astronautical Congress, Naples, Italy. Copyright 2012 by the International Astronautical Federation. All rights reserved. IAC-12-B4,2,11,x15102 ATTITUDE DYNAMICS ANALYSIS OF AALTO-1 SATELLITE DURING D