Real-Time Navigation Using the Global Positioning System

Document Type

Article

Publication Date

1-1995

Publication Title

IEEE Aerospace and Electronic Systems Magazine

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.

Original Citation

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.

DOI

10.1109/62.370460

Volume

10

Issue

1

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