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Accession Number:

AD0485001

Title:

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

Personal Author(s):

Staffanson, Forrest L.

Corporate Author:

WHITE SANDS MISSILE RANGE NM FLIGHT SIMULATION LAB

Report Date:

1960-07-01

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.

Pages:

0054

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

Identifiers:

MANIFOLDS(MATHEMATICS)

Subject Categories:

Guided Missile Trajectories, Accuracy and Ballistics

Ballistics

File Size:

0.00MB

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