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An Application of Kalman Filtering and Time Averaging to Inertial Guidance Evaluation |
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| Authors: | Rosenthal PL Brownlow JD |
| Institution: | Lockheed-California Company P.O. Box 551 D/72-51, B/310, P/B-6 Burbank, CA 91520; |
| Abstract: | A method is developed for estimating circular error probable values and circular error probable rate values of an inertial navigation system using the concepts of Kalman filtering and time averaging. |
| Keywords: | |