Research the decorrelated pseudo-range approach for use in the tightly-coupled GPS/SINS integration system
ACTA AERONAUTICA ET ASTRONAUTICA SINICA -SERIES A AND B- ; 16 , 6 ; 707-710
1995-01-01
4 pages
Article (Journal)
Unknown
DDC: | 629.13 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Investigation of tightly coupled SINS/GPS integration midcourse guidance for air-to-air missiles
British Library Online Contents | 1998
|Tightly-coupled GPS/UWB Integration
Online Contents | 2010
|Quasi‐tightly Coupled GNSS‐INS Integration
Online Contents | 2015
|