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Minimizing Interference in Simultaneous Operations between GPS and Other Instrumentation SystemsKujiraoka, Scott, Troublefield, Robert, Fielder, Russell 10 1900 (has links)
Currently many airborne platforms (missiles, targets, and projectiles) contain multiple instrumentation systems to cover the functions of GPS and either telemetry, beacon tracking and/or flight termination. Most of these platforms are not very large, so mounting of various antennas to support these functions are physically close to each other. As a result, unwanted interference (in the form of RF coupling between them) is unavoidable. This paper will discuss the design considerations involved to minimize this interference as well as some lessons learned with its implementation.
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Imposing management control mechanisms on public programs : a comparison of the Polaris and space station programsAbraham, Douglas Scott 08 1900 (has links)
No description available.
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Study of forces and moments on wing-bodies at high incidenceJohnson, G. A. January 1987 (has links)
No description available.
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Estimation for homing guidanceKee, Ronald James January 1992 (has links)
No description available.
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Application of optimal control to bank-to-turn CLOS guidanceRoddy, D. J. January 1985 (has links)
No description available.
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Modern filter-controllers for bank-to-turn CLOS guidanceFleming, Ronald John January 1987 (has links)
No description available.
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Kill vehicle effectiveness for boost phase interception of ballistic missilesBardanis, Florios. January 2004 (has links) (PDF)
Thesis (M.S.)--Naval Postgraduate School, 2004. / Title from title screen (viewed Nov. 10, 2004). "June 2004." Electronic book. Includes bibliographical references (p. 49-50). Also issued in paper format.
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Acquisition of threat-representative ballistic missile targets /Esquibel, Jerry E. January 2002 (has links) (PDF)
Thesis (M.S. in Program Management)--Naval Postgraduate School, December 2002. / Thesis advisor(s): David F. Matthews, John F. Phillips. Includes bibliographical references (p. 75-81). Also available online.
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Low-frequency describing function models for the Atlas missile thrust chamber electrohydraulic position servo with application to determining rigid-body and propellant-sloshing limit cyclesHermann, Fred William, January 1968 (has links)
Thesis (M.S.)--University of Wisconsin--Madison, 1968. / eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references.
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Khrushchev, Castro and Kennedy : motivation, intention, and the creation of a crisis /Pickering, Robin R. January 1900 (has links)
Thesis (M.A.)--Humboldt State University, 2006. / Includes bibliographical references (leaves 147-154). Also available via Humboldt Digital Scholar.
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