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