DocumentCode
1794764
Title
Design of combination damper of an inertial attitude sensor
Author
Sun Li ; Liang Lu ; Lin Song
Author_Institution
Beijing Inst. of Control Eng., Beijing, China
fYear
2014
fDate
8-10 Aug. 2014
Firstpage
12
Lastpage
15
Abstract
To meet requirements of both satellite and Inertial Attitude Sensor(IAS), combination damper is used. First, the fundamental structure of combination damper is presented in this paper. Second, to validate the effect of design, the characteristic of combination damper of 3+1S mode IAS is analyzed by finite element model. Last, the result of experimental verification is provided.
Keywords
artificial satellites; attitude measurement; electric sensing devices; finite element analysis; inertial navigation; shock absorbers; 3+1S mode IAS; combination damper design; finite element model; inertial attitude sensor; satellite; Analytical models; Metals; Resonant frequency; Rubber; Satellites; Shock absorbers; Vibrations;
fLanguage
English
Publisher
ieee
Conference_Titel
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location
Yantai
Print_ISBN
978-1-4799-4700-3
Type
conf
DOI
10.1109/CGNCC.2014.7007212
Filename
7007212
Link To Document