Accession Number:

AD0485001

Title:

DETERMINING PARAMETER CORRECTIONS ACCORDING TO SYSTEM PERFORMANCE - A METHOD AND ITS APPLICATION TO REAL-TIME MISSILE TESTING,

Descriptive Note:

Corporate Author:

WHITE SANDS MISSILE RANGE NM FLIGHT SIMULATION LAB

Personal Author(s):

Report Date:

1960-07-01

Pagination or Media Count:

54.0

Abstract:

Contents A Hypothetical System Deviation of Motion due to Variations in Inatial Conditions and Parameters The Sensitivity Equations Solving for the Variations in Initial Conditions and Parameters Correction for Higher Order Terms The Effect of Noise Ideal Case and Summary of Conditions and Characteristics.

Subject Categories:

  • Guided Missile Trajectories, Accuracy and Ballistics
  • Ballistics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE