Document Type
Article
Publication Date
4-1995
Publication Title
IEEE Transactions on Aerospace and Electronic Systems
Abstract
The complexity of the design of a Global Positioning System (GPS) user segment, as well as the performance demanded of the components, depends on user requirements such as total navigation accuracy. Other factors, for instance the expected satellite/vehicle geometry or the accuracy of an accompanying inertial navigation system can also affect the user segment design. Models of GPS measurements are used to predict user segment performance at various levels. Design curves are developed which illustrate the relationship between user requirements, the user segment design, and component performance.
Repository Citation
Dougherty, John J.; El-Sherief, Hossny; Simon, Daniel J.; and Whitmer, Gary A., "GPS Modeling for Designing Aerospace Vehicle Navigation Systems" (1995). Electrical and Computer Engineering Faculty Publications. 132.
https://engagedscholarship.csuohio.edu/enece_facpub/132
Original Citation
Dougherty, J.J.; El-Sherief, H.; Simon, D.J.; Whitmer, G.A. (1995). GPS modeling for designing aerospace vehicle navigation systems. Aerospace and Electronic Systems, IEEE Transactions on, 31(2), 695-705, doi: 10.1109/7.381917.
DOI
10.1109/7.381917
Version
Postprint
Publisher's Statement
© 1995 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other users, including reprinting/ republishing this material for advertising or promotional purposes, creating new collective works for resale or redistribution to servers or lists, or reuse of any copyrighted components of this work in other works.
Volume
31
Issue
2
Included in
Electrical and Computer Engineering Commons, Navigation, Guidance, Control and Dynamics Commons
