Satellite attitude stabilization using fluid rings

2009 ◽  
Vol 208 (1-2) ◽  
pp. 117-131 ◽  
Author(s):  
K. D. Kumar
Author(s):  
Ikechukwu Ofodile ◽  
Nkemdilim Ofodile-Keku ◽  
Paul Jemitola ◽  
Gholamreza Anbarjafari ◽  
Andris Slavinskis

2002 ◽  
Vol 39 (5) ◽  
pp. 755-760 ◽  
Author(s):  
K. D. Kumar ◽  
T. Yasaka

Author(s):  
Aleksandr Yu. Aleksandrov ◽  
◽  
Natalya R. Andriyanova ◽  
Aleksey A. Tikhonov ◽  
◽  
...  

A dynamically symmetric satellite in a circular orbit of small inclination is considered. The problem of the Lorentzian stabilization of the satellite in the orbital coordinate system in the indirect equilibrium position is solved under the conditions of the perturbing effect of the gravitational torque. To solve this problem, which is characterized by incomplete control, a method of averaging differential equations is developed. Using the original construction of the unsteady Lyapunov function, we obtain sufficient conditions for the asymptotic stability of the programmed satellite motion mode in the form of constructive inequalities with respect to the control parameters.


2007 ◽  
Vol 40 (7) ◽  
pp. 587-590 ◽  
Author(s):  
Nobutada Sako ◽  
Yoichi Hatsutori ◽  
Takashi Tanaka ◽  
Takaya Inamori ◽  
Shinichi Nakasuka

2017 ◽  
Vol 40 (5) ◽  
pp. 1304-1313 ◽  
Author(s):  
Senqiang Zhu ◽  
Danwei Wang ◽  
Qiang Shen ◽  
Eng Kee Poh

2019 ◽  
Vol 160 ◽  
pp. 240-250 ◽  
Author(s):  
Caoqun Luo ◽  
Hao Wen ◽  
Dongping Jin

2013 ◽  
Vol 6 (5) ◽  
pp. 767-772 ◽  
Author(s):  
薛旭成 XUE Xu-cheng ◽  
傅瑶 FU Yao ◽  
韩诚山 HAN Cheng-shan

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