Computer simulated missile-target engagement with a Luenberger Observer and a ground observer

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Authors
Painter, Gerald L.
Subjects
Missle
Proportional navigation
Luenberger Observer Kalman Filter
Advisors
Titus, Harold A.
Date of Issue
1991-06
Date
June 1991
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
The technique of proportional navigation is applied to a three dimensional missile-target engagement model. A Luenberger observer is developed to reduce the effects of noise or jamming to the missile's seeker head. A ground observer which computes the deviations in target position and velocity and uplinks the deviations to the missile is also evaluated using the Kalman Filter theory to determine the benefits of the additional information provided to the missile.
Type
Thesis
Description
URI
https://hdl.handle.net/10945/26424
Series/Report No
Department
Department of Electrical and Computer Engineering
Organization
Naval Postgraduate School
Identifiers
NPS Report Number
Sponsors
Funder
Format
96 p.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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