自动化与信息科学期刊
每年出版 12 期
ISSN 打印: 1064-2315
ISSN 在线: 2163-9337
SJR:
0.173
SNIP:
0.588
CiteScore™::
2
Indexed in
Satellite Correction Equations for a Strapdown Inertial System
卷 29,
册 1, 1997,
pp. 91-99
DOI: 10.1615/JAutomatInfScien.v29.i1.110
摘要
Equations for satellite correction of an aircraft strapdown inertial navigation system are given. Structure of equations that is suitable for estimating the error vector using a triangular Kalman filter (square-root filter) is specified. The possibility of providing the observability and obtaining estimation of the basic elements of the vector of state under the conditions of a horizontal linear flight is considered.
对本文的引用
-
Miniature Inertial Measurement Unit, in Space Microsystems and Micro/nano Satellites, 2018. Crossref
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