Design and Dynamic Simulation of Hinged Deployable Configuration Spacecraft

Abstract

Abstract: Based on modular design idea of the spacecraft structure, a hinged deployable configuration for the spacecraft was designed. The virtual prototyping model of modular body and solar panels was established with virtual prototyping technology. And the influence of three deployment sequences of modular body and solar panels on attitude of the spacecraft in the weightless space environment were analyzed, including the modular body and solar panels deployed simultaneously, the modular body deployed after the solar panels, and the solar panels deployed after the modular body. Meanwhile, the influences of different torsion spring parameters on attitude angle and deployment time were compared.

Key words: Modular design, Hinge connection, Deployable mechanism, Solar sail, Attitude control, Dynamic simulation, Spacecraft design

MA Shang-Jun, LIU Geng, LUO Hao. Design and Dynamic Simulation of Hinged Deployable Configuration Spacecraft[J]. Chinese Space Science and Technology, 2010, 30(6): 49-56.

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References

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