Design and analysis of Coordinated Bank-To-Turn (CBTT) autopilots for Bank-To-Turn (BTT) missiles.
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Authors
Lioulis, Ioannis S.
Subjects
coordinated bank-to-turn autopilots
pitch-yaw-roll uncoupled autopilots
elliptical and circular airframe
linear CBTT autopilots
nonlinear CBTT autopilots
control laws
pitch-yaw-roll uncoupled autopilots
elliptical and circular airframe
linear CBTT autopilots
nonlinear CBTT autopilots
control laws
Advisors
Collins, Daniel J.
Date of Issue
1983-12
Date
December 1983
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
This work addresses the design and analysis of the
Pitch, Yaw and Roll autopilot for application to the
Bank-To-Turn (BTT) missiles. At first, the linear
uncoupled channels were designed and analyzed according to
the desired requirements. Utilizing the uncoupled
channels, the linear coupled autopilots were designed, not
including the inertial, kinematic and aerodynamic
cross-coupling. Then, the nonlinear CBTT autopilots were
designed and analyzed, using the linear CBTT (coordinated
Bank-To-Turn) models, which now have coupled with
kinematic, inertial and aerodynamic cross-coupling. The
minimization of the above kinematic and inertial coupling
and their effects were completed using feedbacks of
angle-of-attack and rate of angle-of-attack in the Pitch
autopilot.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
Copyright is reserved by the copyright owner