Journal
JOURNAL OF THE ASTRONAUTICAL SCIENCES
Volume 60, Issue 3-4, Pages 672-685Publisher
AMER ASTRONAUTICAL SOC
DOI: 10.1007/s40295-015-0068-7
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One method to account for parameters errors in the Kalman filter is to 'consider' their effect in the so-called Schmidt-Kalman filter. This paper addresses issues that arise when implementing a consider Kalman filter as a real-time, recursive algorithm. A favorite implementation of the Kalman filter as an onboard navigation subsystem is the UDU formulation. A new way to implement a UDU Schmidt Kalman filter is proposed. The non-optimality of the recursive Schmidt-Kalman filter is also analyzed, and a modified algorithm is proposed to overcome this limitation.
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