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Zhou Zhicheng (Beijing Institute of Spacecraft Systems Engineering)
Published:
Abstract: This paper presents a method of shock analysis of deployablesolar array.The dynamical model is obtained using the Finite Segment Me-thod.The curves of acting forces on BAPTA and attitude angles of a satel-lite are given by using the software SDFX.
Key words: Solar sail, Spacecraft, Attitude, Dynamics, Analyzing
Zhou Zhicheng (Beijing Institute of Spacecraft Systems Engineering). DEPLOYMENT AND SHOCK ANALYSIS OF SPACECRAFT SOLAR ARRAY[J]. .
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http://zgkj.cast.cn/EN/Y1992/V12/I04/2
