Simulation study of the roll control loop of an operational surface to air missile
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Authors
Hall, David Parkin
Subjects
Digital simulations
Adaptive control
Missile control roll loop
Digitally simulated white noise
Dither
Roll wander
DSL
DSLPLOT
Adaptive control
Missile control roll loop
Digitally simulated white noise
Dither
Roll wander
DSL
DSLPLOT
Advisors
Thaler, George J.
Date of Issue
1973-12
Date
December 1973
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
This thesis studies the roll loop of an operational surface to air missile as an example of a typical self adaptive control system. The missile studied also exhibits a phenomenon called ROLL WANDER, a low frequency oscillation in missile roll orientation. Because of this, the thesis is developed in three major areas of study. First, is the study of the missile roll control loop. Second, is a study of the
phenomenon of ROLL WANDER, with the production of this phenomenon in the computer simulation. Third and finally is the implementation, in the computer simulation, of a self adaptive notch filter to suppress the occurrence of ROLL WANDER.
Type
Thesis
Description
Series/Report No
Department
Electrical Engineering
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
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.