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IMPULSE CONTROL SYSTEM OF UNMANNED SPACECRAFT
IMPULSE CONTROL SYSTEM OF UNMANNED SPACECRAFT
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机译:意外航天器的冲量控制系统
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摘要
An impulse control system of an unmanned spacecraft has connected in-series orientation sensors, including magnetometers, a computer unit, amplifiers and working coils. In the last stages of amplifiers modulators are introduced, for example, pulse-length modulators, which by their outputs are connected to the inputs of working coils.
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