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Thursday, April 23, 2020 | History

4 edition of Optimal guidance law development for an advanced launch system found in the catalog.

Optimal guidance law development for an advanced launch system

Optimal guidance law development for an advanced launch system

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English


Edition Notes

StatementAnthony J. Calise and Martin S.K. Leung.
Series[NASA contractor report] -- NASA CR-4667., NASA contractor report -- NASA CR-4667.
ContributionsLeung, Martin S. K., United States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL17791316M
OCLC/WorldCa33238942

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Optimal guidance law development for an advanced launch system Download PDF EPUB FB2

OPTIMAL GUIDANCE LAW DEVELOPMENT FOR AN ADVANCED LAUNCH SYSTEM Anthony J. Calise* and Martin S. Leung** Georgia Institute of Technology, GA SUMMARY The objective of this research effort was to develop a real-time guidance approach for launch vehicles ascent to orbit injection.

Various analytical approaches combined. Optimal Guidance Law Development for an Advanced Launch System //j P._3 Interim Progress Report 1 December - 15 June June \ \ \ \ \ \ Research Supported by NASA Langley Research Center NASA Grant No.

NAG-I Principal Investigators: Anthony J. Calise & Dewey H. Hodges Research Assistant: Martin S. Leung & Robert R. Bless. Get this from a library. Optimal guidance law development for an advanced launch system: interim progress report.

[Anthony J Calise; Dewey H Hodges; United. Get this from a library. Optimal guidance law development for an advanced launch system: interim progress report, 1 December June [Anthony J Calise; Dewey H Hodges; United States.

National Aeronautics and Space Administration.]. Abstract. The navigation, guidance and control (NGC) system, the brain of the vehicle, is responsible for directing the propulsive forces and stabilizing the vehicle along the desired path to achieve the orbit with the specified : B.

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