Design and on-orbit performance of the attitude determination and control system for the ZDPS-1A pico-satellite

T Xiang, T Meng, H Wang, K Han, ZH Jin - Acta Astronautica, 2012 - Elsevier
The ZDPS-1A pico-satellite, developed by the Zhejiang University, is featured with a three-
axis stabilizing capability. It is 15× 15× 15cm3 cube-shaped satellite with a total mass of 3.5 …

Three-axis attitude control of a small satellite by magnetic PD-like controller integrated with passive pitch bias momentum method

A Sofyali, EM Jafarov - Proceedings of 5th International …, 2011 - ieeexplore.ieee.org
The attitude acquisition problem of a magnetic small satellite under effect of environmental
disturbances is solved by two methods. The first method stabilizes the nonlinear attitude in …

Computational phase portrait analysis of two nonlinear small satellite models

A Sofyali, E Caferov - 2009 4th International Conference on …, 2009 - ieeexplore.ieee.org
Two small satellite models are selected that are subject to gravity gradient in circular, low-
altitude orbits. The second one is passively controlled by a pitch momentum wheel. The aim …

[PDF][PDF] Küçük uydularda doğrusal olmayan yönelme dinamiği ve üç eksende manyetik PD ve kayma kipli kontrolcü tasarımı

A Sofyalı - 2010 - polen.itu.edu.tr
Uzay teknolojisinde yaşanan gelişmelere koşut olarak kabiliyetleri giderek artan küçük
uydulardan gelecekte, günümüzde olduğundan daha fazla ve daha çeşitli uzay görevinde …

[PDF][PDF] DESIGN AND TESTING OF ATTITUDE DETERMINATION SENSORS FOR ESTCUBE-1

J Viru - core.ac.uk
The CubeSat standard was developed in 1999 by California Polytechnic State University
and Stanford University [1]. First CubeSats where mostly developed by universities. In recent …

[引用][C] K 频段测距系统星间高精度指向控制算法

辛宁, 邱乐德, 周钠, 张立华 - 航天器工程, 2016

[引用][C] 喷气/偏置动量轮联合微小卫星三轴稳定控制

刘海颖, 王惠南, 陈志明, 叶伟松 - 系统仿真学报, 2009