Performance data is presented for a sampled data delay-lock-loop incorporating a Kalman predictor. The jitter response due to noise and the deterministic response to aircraft maneuvers are investigated as a function of the Kalman model parameters. The predictor's transient response to step, ramp, and parabolic inputs and the number of iterations required for convergence for typical initialization errors are determined. It is shown how values for the model parameters may be chosen to obtain satisfactory noise, maneuver, and lock-up performance.
A Sampled Data Delay-Lock Loop Implemented as a Kalman Predictor
IEEE Transactions on Aerospace and Electronic Systems ; AES-16 , 6 ; 800-810
1980-11-01
1883669 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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