The Kalman Filter in Transfer Alignment of Airborne Inertial Guidance Systems

doi:https://doi.org/10.21236/ad0851067

The Kalman Filter in Transfer Alignment of Airborne Inertial Guidance Systems

Jr. Sutherland,Gelb Arthur A.,Arthur Arthur-1968-10-01

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TL;DRAbstract

Abstract : The problem of transferring alignment between two airborne inertial navigator platforms is treated using the Kalman filter approach. The important parameters are identified and exercised over a reasonable range to establish accuracy trade-offs. Suggestions are provided for improving the accuracy of Kalman filter transfer alignment through more complex maneuvers of the carrying aircraft.

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Abstract : The problem of transferring alignment between two airborne inertial navigator platforms is treated using the Kalman filter approach. The important parameters are identified and exercised over a reasonable range to establish accuracy trade-offs. Suggestions are provided for improving the accuracy of Kalman filter transfer alignment through more complex maneuvers of the carrying aircraft.

Keywords

Kalman filterInertial frame of referenceInertial measurement unitInertial navigation systemComputer scienceTransfer (computing)Environmental scienceRemote sensing

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