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Orbit determination solution to non-Markov gravity...
Conference

Orbit determination solution to non-Markov gravity error problem

Abstract

Sequential orbit determination refers to orbit determination which is sequential with time. Computational tractability is enabled in part by requiring that all modeling error processes be Markov with time. The Markov principle asserts that if the state of a process is known at current time, then the conditional probability of any future event is not changed if additional information about the past is made available. Error processes with strong …

Authors

Wright JR

Volume

87

Pagination

pp. 1153-1172

Publication Date

January 1, 1994

Conference proceedings

Advances in the Astronautical Sciences

Issue

2

ISSN

0065-3438