Hidden oscillations in stabilization system of flexible launcher with saturating actuators

Links

http://www.scopus.com/inward/record.url?partnerID=HzOxMe3b&scp=84899694650&origin=inward

DOI

https://doi.org/10.3182/20130902-5-de-2040.00040
Final published version

In the paper the attitude stabilization system of the unstable flexible launcher with saturating input is considered. It is demonstrated that due to actuator saturation the system performance can significantly degrade. The analytical-numerical method is applied to demonstrate possibility of hidden oscillations and localize their attractor.

Original language	English
Title of host publication	19th IFAC Symposium on Automatic Control in Aerospace, ACA 2013 - Proceedings
Publisher	International Federation of Automatic Control
Pages	37-41
Number of pages	5
Edition	PART 1
ISBN (Print)	9783902823465
DOIs	https://doi.org/10.3182/20130902-5-de-2040.00040
State	Published - 2013
Event	19th IFAC Symposium on Automatic Control in Aerospace, ACA 2013 - Wurzburg, Germany Duration: 2 Sep 2013 → 6 Sep 2013

Publication series

Name	IFAC Proceedings Volumes (IFAC-PapersOnline)
Number	PART 1
Volume	19
ISSN (Print)	1474-6670

Conference

Conference	19th IFAC Symposium on Automatic Control in Aerospace, ACA 2013
Country/Territory	Germany
City	Wurzburg
Period	2/09/13 → 6/09/13

Scopus subject areas

Control and Systems Engineering

Research areas

Actuator saturation, Flexible structure control, Launcher, Oscillations

ID: 7412067