Constrained control of very flexible aircraft using reference and extended command governors

This paper presents a control scheme composed of a closed loop system consisting of a dynamic inversion inner loop controller and a proportional, integral, derivative outer loop controller augmented with either a reference or an extended command governor that is developed for very flexible aircraft...

Full description

Saved in:
Bibliographic Details
Published in2013 American Control Conference pp. 1608 - 1613
Main Authors Dillsaver, Matthew J., Kalabic, Uros V., Kolmanovsky, Ilya V., Cesnik, Carlos E. S.
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.06.2013
Subjects
Aerodynamics
Aircraft
Atmospheric modeling
Closed loop systems
Electrocardiography
Mathematical model
Vectors
Online AccessGet full text
ISBN1479901776
9781479901777
ISSN0743-1619
DOI10.1109/ACC.2013.6580065

Cover

More Information
Summary:This paper presents a control scheme composed of a closed loop system consisting of a dynamic inversion inner loop controller and a proportional, integral, derivative outer loop controller augmented with either a reference or an extended command governor that is developed for very flexible aircraft flight trajectory control. The governors enforce curvature limits, which are directly proportional to bending moment, on a very flexible aircraft model following a flight path angle set-point command.
ISBN:1479901776
9781479901777
ISSN:0743-1619
DOI:10.1109/ACC.2013.6580065