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):

• Isom, Larmon 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

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