Abstract
A best linear unbiased estimate (BLUE) of the input process which characterizes a pilot-induced maneuver is developed for the case of the one-dimensional Kalman filter. This approach is utilized to yield a recursive implementation of the adaptive Kalman filter that is identical to that obtained by P.L. Bogler in the above mentioned paper (see ibid., vol.AES-23, no.3, p.298-310, May 1987). >
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More From: IEEE Transactions on Aerospace and Electronic Systems
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