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    • 1. 发明授权
    • Battery regulated bus spacecraft power control system
    • 电池调节总线航天器功率控制系统
    • US5530335A
    • 1996-06-25
    • US60103
    • 1993-05-11
    • Darwin K. DeckerCharles B. Loftis, Jr.
    • Darwin K. DeckerCharles B. Loftis, Jr.
    • G05F1/67H01M10/46H02J4/00H02J7/35
    • G05F1/67H01M10/465H02J4/00H02J7/35Y02E10/566Y02E10/58Y10S136/293
    • A system for supplying d.c. power to an electrical load, in which such load includes a rechargeable battery, is characterized by a plurality of power sources connected in common to the electrical load, wherein the current generated by the multiple power sources is combined to supply such electrical load. Each of the power sources includes a solar panel and a controlled variable transconductance device, such as a Buck converter, connected in electrical series circuit. A digital processor, including a stored program, coupled to the control inputs of the variable transconductance devices, selectively individually sets the duty cycle of each transconductance device under control of a stored program, whereby the electrical power supplied by said power sources to said electrical load is individually controlled by the digital processor.
    • 提供直流电源的系统 其中这种负载包括可再充电电池的电负载的功率的特征在于多个电源连接到电负载,其中由多个电源产生的电流被组合以提供这种电负载。 每个电源包括连接在电气串联电路中的太阳能电池板和控制可变跨导装置,例如降压转换器。 耦合到可变跨导装置的控制输入的数字处理器,包括存储的程序,在存储的程序的控制下,选择性地单独地设置每个跨导装置的占空比,由此由所述电源提供给所述电负载的电力 由数字处理器单独控制。