Accession Number : AD0854361

Title :   An Automated Computation of the Circular Error Probability for an Inertial Guidance System,

Corporate Author : ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL GUI DANCE AND CONTROL DIRECTORATE

Personal Author(s) : Isom, Larmon S.

Report Date : 03 FEB 1969

Pagination or Media Count : 114

Abstract : This report discusses in detail a digital computer program to evaluate the circular error probability of a weapon's inertial guidance system. It includes a derivation of equations and an example of a typical circular error probability case study. (Author)

Descriptors :   (*SURFACE TO SURFACE MISSILES, INERTIAL GUIDANCE), (*CIRCULAR ERROR PROBABLE, COMPUTER PROGRAMMING), MATHEMATICAL MODELS, MISS DISTANCE, GUIDED MISSILE TRAJECTORIES, ERRORS, IMPACT PREDICTION, FLOW CHARTING, SUBROUTINES.

Subject Categories : Computer Programming and Software
      Surface-launched Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE