太阳帆推进任务的快速仿真方法

doi:10.3969/j.issn.1674-1579.2016.02.002

Abstract

Abstract: Abstract：Dynamic of solar sail and method of trajectory design have been analyzed. Then the control forces calculated by the control strategy are added into the STK orbit propagator, which is realized through the STK plugin coded by MATLAB. The simulation results show that the methods proposed can realize expeditiously and efficiently that STK/MATLAB coordinated work to neatly support control simulation of special force model such as solar sail dynamic, and the abundant capabilities of STK are suitable for designing and analysising the complex space mission.

Key words: Keywords：complex trajectory design, STK, solar sail, low thrust control

CLC Number:

V529.1

QIAN Hang, ZHENG Jian-Hua, WU Xia, GAO Dong, LIU Yu-Fei. Method of Mission Analysis for Solar Sail Exploration Based on STK[J]., 2016, 42(2): 8-13.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2016.02.002

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2016/V42/I2/8

References

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[4]	QIAN Hang, ZHENG Jian-Hua. Optimization Algorithm for Interplanetary Transfer Trajectories of SolarSail Spacecraft [J]. , 2012, 38(1): 18-22.
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Method of Mission Analysis for Solar Sail Exploration Based on STK

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