Title :
Design and analysis of the root stiffness mechanism of the deploying and retracting mast
Author :
Liu, Heping ; Luo, Ani ; Zhang, Lixun
Author_Institution :
Sch. of Mech. & Electr. Eng., Harbin Eng. Univ., Harbin, China
Abstract :
According to working principle of the deploying and retracing mast, this paper presents that the mast needs to be stiffened by a root stiffness mechanism. The double-slider mechanism with a spring is designed as the root stiffness mechanism. Then motion of the root stiffness mechanism is studied to set up vibrating equation of slider 2 based on the Lagrange equation. Displacement and velocity expression of slider 2 are obtained. At last, the Matlab program is used to check correctness of theory analysis. Elastic coefficient of spring and length of bars are selected by the program.
Keywords :
aerospace components; bars; elastic constants; springs (mechanical); vibrations; Lagrange equation; Matlab program; bars; deploying mast; double-slider mechanism; elastic coefficient; retracting mast; root stiffness mechanism; spring; vibrating equation; Bars; Cables; Design engineering; Equations; Lagrangian functions; Orbits; Space exploration; Space technology; Spaceborne radar; Springs; Deploy and retract mast; equation of motion; stiffness;
Conference_Titel :
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-7737-1
DOI :
10.1109/MACE.2010.5536170