An Integrated DGPS/INS Navigation System for a Ballistic Missile: Design and Flight Test Results

Author:

COFFEE JOHN R.,MAGANTY PRASAD

Publisher

Institute of Navigation

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Reference15 articles.

1. Use of the Global Positioning System for Evaluating Inertial Measurement Unit Errors;Dougherty;Journal of Guidance, Control, and Dynamics,MayJune 1994

2. Moore , T. Rudolph , K. Ziolkowski , F. Luckau , A. Use of the GPS Aided Inertial Navigation System in the Navy Standard Missile for the BMDO/Navy LEAP Technology Demonstration Program , Proceedings of ION GPS-95, the 8th International Technical Meeting of the Satellite Division of The Institute of Navigation, Palm Springs, CA September 1995 363 71

3. Beck , G. Dare , J. Kaiser , J. Bedoya , C. Jenkins , T. Howe , P. GPS Exploitation for Precision Targeting: Tactical Applications , Proceedings of the 49th Annual Meeting of The Institute of Navigation, Cambridge, MA June 1993 183 92

4. Harris , R. Setterlund , R. Advanced Maneuvering Re-entry Vehicle Guidance , Proceedings of the 49th Annual Meeting of The Institute of Navigation, Cambridge, MA June 1993 537 42

5. Precision Strike Concepts Exploiting Relative GPS Techniques;Schmidt;NAVIGATION, Journal of The Institute of Navigation,Spring 1994

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