Author

Mark E. Ennis

Date of Award

3-1994

Document Type

Thesis

Degree Name

Master of Science

Department

Department of Electrical and Computer Engineering

First Advisor

Randall Paschall, PhD

Abstract

An extended Kalman filter is used to predict a kinetic kill zone for use in aircraft self defense versus homing missiles. The analysis is limited to an in-the-plane analysis and focuses on finding the model parameters which have the largest impact on the predicted kill zone. No attempt is made to optimize the design of the filter model itself. The analysis computes the kill zone relative to an assumed aircraft trajectory using strictly filter computed statistics. No Monte-Carlo simulations are used throughout the thesis. The filter assumed to be on the evading aircraft, uses an onboard laser radar (ladar) to provide measurements of aircraft-to-missile relative range, range-rate, line-of-sight and line-of -sight rate. The missile is assumed to be in a post burnout coast-to-intercept phase of flight.

AFIT Designator

AFIT-GE-GEO-94M-01

DTIC Accession Number

ADA278705

Comments

The author's Vita page is omitted.

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