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A NEW METHOD FOR SIMULATING THE ATTITUDE DYNAMICS OF PASSIVELY MAGNETICALLY STABILIZED SPACECRAFT

机译:模拟被动磁稳压航天器姿态动态的新方法

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A new method for simulating the behavior of magnetically permeable material is presented that offers an order of magnitude reduction in simulation run time compared to existing methods with no loss in accuracy. The new method was integrated into a full attitude dynamics simulation of the NASA O/OREOS spacecraft and preliminary comparisons between the simulation results and orbit data are made.
机译:提出了一种模拟磁性可渗透材料的行为的新方法,其提供了与仿真运行时间的幅度减小,而现有方法与准确性没有损失。将新方法集成到NASA O / OREOS航天器的完整姿态动态模拟,并进行了模拟结果和轨道数据之间的初步比较。

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