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Метод адаптивної рекурентної фільтрації вимірювань параметрів космічних об’єктів
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UDC: 681.5.015.44:621.396.96
Publication Language: Russian
Stuc. intelekt. 2008; 13(4):62-73
Abstract: The synthesis of adaptive recurrent filter which is intended for statistical treatment of measurings of space objects parameters movement on the stage of orbital maneuver in the measuring informative systems is considered. Development principle of separation is underlaid. The model of space objects motion is taken into account in a filter, which allowed effectively to carry out authentication of trajectory parameters on the stage of orbital maneuver, and substantially to reduce the run-time error of addition on this stage.
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