Accession Number : AD0848383
Title : Navigational Error Analyses for a Ballistic Missile.
Descriptive Note : Technical publication,
Corporate Author : NAVAL WEAPONS CENTER CHINA LAKE CA
Personal Author(s) : Nuffer, Harold D.
Report Date : DEC 1968
Pagination or Media Count : 169
Abstract : Navigational errors for two ballistic missile navigational systems-one gimbaled and one strapped-down-are analyzed. Equations are derived for studying navigational errors resulting from sensor errors. Navigational errors at end of guidance (burnout) are determined and then propagated to the target by orbit-sensitivity equations. FORTRAN V program listing for each system are presented in Appendixes A and B, respectively. Flow charts for both systems are given in Appendix C. (Author)
Descriptors : *INERTIAL NAVIGATION), (*GUIDED MISSILES, ERRORS, INSTRUMENTATION, NUMERICAL ANALYSIS, COMPUTER PROGRAMS, ACCELEROMETERS, GYROSCOPES, CELESTIAL MECHANICS, STABILIZED PLATFORMS.
Subject Categories : Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE