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Relative position control device by output measurement for one spacecraft in a spacecraft group that forms a formation
Relative position control device by output measurement for one spacecraft in a spacecraft group that forms a formation
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机译:通过输出测量形成航天器组的航天器组中的一个航天器的相对位置控制装置
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摘要
The device has three send/receive antennas (A1-A3) installed on an observation satellite of a group of satellites and sending/receiving radio frequency signals. A measurement unit (MM) delivers power sets associated with one of the other satellites. A storage unit (BD) stores cartographic data sets representing powers of the signals received by the antennas based on transmission directions. A processing unit (MT) compares each power set with the data sets to estimate the directions of the signals sent by the satellites with respect to a reference system tied to the observation satellite.
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