A computer analysis of proportional navigation and command to line of sight of a command guided missile for a point defence system

Approved for public release; distribution is unlimited. / This thesis compares two types of command guidance to be used by a point defense system: Proportional Navigation and Command to Line Of Sight (CLOS). The system block diagram was first defined. The necessary transfer functions were derived. Two forward time models were evaluated, one for each guidance method, using state variable analysis. Two three dimensional scenarios were defined and their results used to compare the two methods. Parameters considered in the comparison were miss distance and acceleration load on the missile.

Identiferoai:union.ndltd.org:nps.edu/oai:calhoun.nps.edu:10945/38511
Date12 1900
CreatorsPeppas, Dimitrios Ioannis
ContributorsTitus, Harold A., Cristi, Roberto, Naval Postgraduate School (U.S.), Department of Electrical and Computer Engineering
PublisherMonterey, California. Naval Postgraduate School
Source SetsNaval Postgraduate School
Languageen_US
Detected LanguageEnglish
TypeThesis
RightsCopyright is reserved by the copyright owner.

Page generated in 0.0011 seconds