Related Books
Language: en
Pages: 197
Pages: 197
Type: BOOK - Published: 2018-03-15 - Publisher: Universitätsverlag der TU Berlin
This thesis investigates a new concept for the flexible design and verification of an ADCS for a nanosatellite platform. In order to investigate guidelines for
Language: en
Pages: 190
Pages: 190
Type: BOOK - Published: 2018-11-14 - Publisher: Cambridge Scholars Publishing
This book explores CubeSat technology, and develops a nonlinear mathematical model of a spacecraft with the assumption that the satellite is a rigid body. It pl
Language: en
Pages: 111
Pages: 111
Type: BOOK - Published: 2001-09 - Publisher:
The NPSAT1 satellite uses an active magnetic torque rod system, with a magnetometer for attitude determination, to maintain 3-axis stabilization, with a slightl
Language: en
Pages: 36
Pages: 36
Type: BOOK - Published: 1970 - Publisher:
A strapdown inertial reference system and an onboard digital computer can be used to change the attitude of a spacecraft over large angles in an arbitrary direc
Language: en
Pages: 256
Pages: 256
Type: BOOK - Published: 2006 - Publisher:
