An innovative scheme for SINS/GPS ultra-tight integration system with low-grade IMU
- 1 December 2012
- journal article
- Published by Elsevier BV in Aerospace Science and Technology
- Vol. 23 (1), 452-460
- https://doi.org/10.1016/j.ast.2011.10.004
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Design and analysis for an innovative scheme of SINS/GPS ultra‐tight integrationAircraft Engineering and Aerospace Technology, 2010
- A Novel Architecture for Ultra-Tight HSGPS-INS IntegrationThe Journal of Global Positioning Systems, 2008
- Sensitivity and Performance Analysis of Doppler-Aided GPS Carrier-Tracking LoopsNAVIGATION: Journal of the Institute of Navigation, 2005
- Impact of inertial system quality on GPS-inertial performance in a jamming environmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987