Accession Number : AD0485001

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

Corporate Author : WHITE SANDS MISSILE RANGE NM FLIGHT SIMULATION LAB

Personal Author(s) : Staffanson, Forrest L.

Report Date : JUL 1960

Pagination or Media Count : 54

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.

Descriptors :   (*GUIDED MISSILE TRAJECTORIES, EXTERIOR BALLISTICS), (*FLIGHT PATHS, GUIDED MISSILES), MATHEMATICAL MODELS, FLIGHT TESTING, REAL TIME, SIMULATION, MOTION, MATHEMATICAL ANALYSIS, NONLINEAR DIFFERENTIAL EQUATIONS, THEORY, GUIDED MISSILE MODELS, VECTOR ANALYSIS, APPROXIMATION(MATHEMATICS), MOMENTS, ERRORS, DATA PROCESSING, FLIGHT SIMULATORS.

Subject Categories : Guided Missile Traj, Accuracy and Ballistics
      Ballistics

Distribution Statement : APPROVED FOR PUBLIC RELEASE