Accession Number:

AD0854361

Title:

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

Descriptive Note:

Corporate Author:

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

Personal Author(s):

Report Date:

1969-02-03

Pagination or Media Count:

114.0

Abstract:

This report discusses in detail a digital computer program to evaluate the circular error probability of a weapons inertial guidance system. It includes a derivation of equations and an example of a typical circular error probability case study. Author

Subject Categories:

  • Computer Programming and Software
  • Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE