Controller design for lateral manoeuvres in electromagnetic wind tunnels

dc.creator	Koumboulis, F. N.	en
dc.creator	Skarpetis, M. G.	en
dc.date.accessioned	2015-11-23T10:36:09Z
dc.date.available	2015-11-23T10:36:09Z
dc.date.issued	1996
dc.identifier.uri	http://hdl.handle.net/11615/29807
dc.description.abstract	The roll angle, the yaw angle and the side-slip position of test aircrafts in electromagnetic wind tunnels, are independently controlled. The problem is proven to be always solvable by applying a static state feedback law involving aerodynamic and electromagnetic variables. The general forms of the static controllers, solving the problem, as well as the resulting closed loop system, are derived. The stability of the closed loop is guaranteed.	en
dc.source.uri	http://www.scopus.com/inward/record.url?eid=2-s2.0-0030372976&partnerID=40&md5=dff3c4a0204b72d7e2a813d877ab3e2c
dc.subject	Aerodynamics	en
dc.subject	Aircraft	en
dc.subject	Closed loop control systems	en
dc.subject	Feedback	en
dc.subject	Motion control	en
dc.subject	State space methods	en
dc.subject	System stability	en
dc.subject	Torque	en
dc.subject	Electromagnetic wind tunnels	en
dc.subject	Static state feedback law	en
dc.subject	Wind tunnels	en
dc.title	Controller design for lateral manoeuvres in electromagnetic wind tunnels	en
dc.type	conferenceItem	en

Files in questo item

Files	Dimensione	Formato	Mostra
Nessun files in questo item.