Controller design for a trajectory tracking missile by using inverse dynamics method
Date
1996
Authors
Editor(s)
Advisor
Morgül, Ömer
Supervisor
Co-Advisor
Co-Supervisor
Instructor
Source Title
Print ISSN
Electronic ISSN
Publisher
Volume
Issue
Pages
Language
English
Type
Journal Title
Journal ISSN
Volume Title
Series
Abstract
In this thesis, a controller for a missile desired to track a given trajectory is designed by using the nonlinear inverse dynarnics(NID) method. The nonlinear dynamic equations describing the motion of the missile are linearized from input to the output by using the NID method without any need to the linearizing approximations as in the conventional linearizing method. Hence, designed controller for the linearized system stabilizes the nonlinear system over entire range of the operating points. Two approaches used in the controller design are presented in this thesis.
Course
Other identifiers
Book Title
Keywords
Degree Discipline
Electrical and Electronic Engineering
Degree Level
Master's
Degree Name
MS (Master of Science)