Flexible attitude control design and on-orbit performance of the ZDPS-2 satellite

ZDPS-2, the 2nd generation nano-satellites designed and manufactured by Microsat Research Center of Zhejiang University, were successfully launched by the new generation rocket CZ-6 on Sep 20th, 2015. They are two 20kg identical nano-satellites (ZDPS-2-A and ZDPS-2-B) with a large deployable mechani...

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Veröffentlicht in:	Acta astronautica 2017-01, Vol.130, p.147-161
Hauptverfasser:	Deng, Shengchao, Meng, Tao, Wang, Hao, Du, Chaoyu, Jin, Zhonghe
Format:	Artikel
Sprache:	eng
Schlagworte:	ADCS Aerospace environments Attitude control Attitude stability Control stability Damping Deployable structures Design Design engineering Earth axis Earth stations Field of view Flexible deployable mechanism Formation flying Infrared cameras Infrared detectors Nano-satellite Nanosatellites New technology Nonlinear programming Propulsion Robust control Rockets Satellite attitude control Satellites Sensors Space environment Spacecraft Studies Systems design Three-axis stabilization ZDPS-2
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