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Article
Real-Time Navigation Using the Global Positioning System
IEEE Aerospace and Electronic Systems Magazine
  • Daniel J. Simon, Cleveland State University
Document Type
Article
Publication Date
1-1-1995
Abstract
This paper presents the results of an investigation of the application of the Global Positioning System (GPS) to real-time integrated missile navigation. We present quantifiable measures of navigation accuracy as a function of GPS user segment parameters. These user segment parameters include antenna phase response accuracy, single versus dual frequency, and Kalman filter structure and size. We also formulate some new phase-locked loop (PLL) filter designs for application in GPS receivers, and demonstrate their superiority over more conventional filters
Comments

Also published in TRW Systems Integration Group Technology Review, vol. 2, no. 1, pp. 57-72, Summer 1994.

DOI
10.1109/62.370460
Citation Information
D. Simon and H. El-Sherief. (1995). Real-Time Navigation Using the Global Positioning System. IEEE Aerospace and Electronic Systems Magazine, 10(1), 31-37.