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Calculated and tabulated gain is always maximum gain, that is gain along the boresight. the attitude control system has the task of pointing spacecraft antennas, and there is error in the process. therefore this loss accounts for the off boresight angle resulting from the error in antenna pointing.

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Calculated and tabulated gain is always maximum gain, that is gain along the boresight. the attitude control system has the task of pointing spacecraft antennas, and there is error in the process. therefore this loss accounts for the off boresight angle resulting from the error in antenna pointing.

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