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Stellar-inertial guidance capabilities for advanced ICBM

Rounds, S. F.; Marmar, G.
IN: Guidance and Control Conference, Gatlinburg, TN, August 15-17, 1983, Collection of Technical Papers (A83-41659 19-63). New York, American Institute of Aeronautics and Astronautics, 1983, p. 849-855.
This paper will discuss the capabilities and advantages of stellar-inertial guidance systems, particularly as they apply to the requirements of advanced ICBM systems. The principles of stellar-inertial guidance will be developed. Examples will be given, both simplified examples as aids in understanding the concepts, as well as realistic examples demonstrating the accuracy improvements provided by a stellar update. The capabilities of stellar-inertial guidance in meeting the requirements of dormancy, quick reaction, and basing adaptability, in addition to accuracy will be presented. Finally, the performance of a stellar sensor in a hostile environment will be discussed.

AND:

Strategic inertial navigation systems - high-accuracy inertially stabilized platforms for hostile environments

This paper appears in:
Control Systems, IEEE
Date of Publication: Feb. 2008
Author(s): Wang, H.G.
Boeing Co., Chicago
Williams, T.C.
Volume: 28, Issue: 1
On Page(s): 65 - 85
Product Type: Journals & Magazines
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