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Spacecraft gyro calibration system

  • US 20050108884A1
  • Filed: 11/26/2003
  • Published: 05/26/2005
  • Est. Priority Date: 11/26/2003
  • Status: Active Grant
First Claim
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1. A method of calibrating a gyro of a spacecraft comprising:

  • determining a roll gyro bias residual in response to a yaw attitude residual; and

    calibrating the gyro in response to said roll gyro bias residual.

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