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Reduction of the Effect of Component Errors in Inertial Navigation Systems
Published online by Cambridge University Press: 18 January 2010
Abstract
The basic concept of case and cluster rotation in inertial navigation (IN) systems is introduced, and the reduction in the errors caused by changes in gyro and accelero-meter biases is illustrated. The general properties of cluster rotated systems are summarized and it is concluded that, although errors inside the Schuler loops may be drastically reduced by rotation, care must be taken to avoid error sources outside the loops.
- Type
- Inertial Navigation Systems for the Airlines
- Information
- Copyright
- Copyright © The Royal Institute of Navigation 1969
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