Tightly coupled GPS/INS integration for missile applications
- 31 October 2004
- journal article
- Published by Elsevier BV in Aerospace Science and Technology
- Vol. 8 (7), 627-634
- https://doi.org/10.1016/j.ast.2004.07.003
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- GPS/INS-StreamlinedNAVIGATION: Journal of the Institute of Navigation, 2002
- Real-time differential carrier phase GPS-aided INSIEEE Transactions on Control Systems Technology, 2000
- A Nonlinear Observer for Integration of GPS and Inertial Navigation SystemsModeling, Identification and Control: A Norwegian Research Bulletin, 2000
- Architectures and GPS/INS integration: impact on mission accomplishmentIEEE Aerospace and Electronic Systems Magazine, 1992