Flight control system design via static output feedback: LMI-approach

Author

Komnatska, M.M.

Author_Institution

Aircraft Control Syst. Dept., Nat. Aviation Univ., Kiev, Ukraine

fYear

2013

fDate

15-17 Oct. 2013

Firstpage

184

Lastpage

186

Abstract

A contemporary approach of flight control system design via static output feedback design is proposed. The static output feedback is formulated in terms of linear matrix inequalities. The obtained solution guarantees stabilization of unmanned aerial vehicle (UAV) during flight mission. During flight envelope the unmanned aerial vehicle is subjected to the external stochastic disturbances. The efficiency of the proposed approach is illustrated by a case study of UAV longitudinal motion.

Keywords

aerospace control; autonomous aerial vehicles; control system synthesis; feedback; linear matrix inequalities; stochastic processes; LMI; UAV longitudinal motion; external stochastic disturbances; flight control system design; flight envelope; flight mission; linear matrix inequalities; static output feedback design; unmanned aerial vehicle stabilization; Aerospace control; Atmospheric modeling; Conferences; Output feedback; Robustness; Unmanned aerial vehicles; Vectors; aircraft control; disturbance attenuation; external disturbances; linear matrix inequality; robustness; static output feedback; unmanned aerial vehicle;

fLanguage

English

Publisher

ieee

Conference_Titel

Actual Problems of Unmanned Air Vehicles Developments Proceedings (APUAVD), 2013 IEEE 2nd International Conference

Conference_Location

Kiev

Print_ISBN

978-1-4799-3305-1

Type

conf

DOI

10.1109/APUAVD.2013.6705320

Filename

6705320