Attitude Resolution for Strapdown Inertial Systems Using Quaternion Methods
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When performing attitude resolution, the quaternion method can be employed to effectively solve attitude determination problems in strapdown inertial systems. This approach typically involves implementing quaternion normalization and integration algorithms to maintain numerical stability while updating orientation parameters. Additionally, we can calculate navigation parameters using fused data from accelerometers and gyroscopes, which requires implementing sensor fusion algorithms like complementary filters or Kalman filters to achieve more precise position and direction determination. These methodologies are crucial for developing robust navigation systems and help researchers better understand and master advanced navigation technologies through practical algorithm implementation.
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