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Design and testing of spacecraft power systems using VTB

机译:使用VTB设计和测试航天器动力系统

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摘要

A study is presented on the design and testing of spacecraft power systems using the virtual test bed (VTB). The interdisciplinary components such as solar array and battery systems were first modeled in native VTB format and validated by experiment data. The shunt regulator and battery charge controller were designed in Simulink according to the system requirements and imported to VTB. Two spacecraft power systems were then designed and tested together with the control systems.
机译:提出了一项关于使用虚拟测试台(VTB)设计和测试航天器动力系统的研究。跨学科组件(例如太阳能电池板和电池系统)首先以本地VTB格式建模,并通过实验数据进行了验证。分流稳压器和电池充电控制器是根据系统要求在Simulink中设计的,并导入到VTB中。然后设计了两个航天器动力系统,并与控制系统一起进行了测试。

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