DocumentCode
425572
Title
A stochastically optimal feedforward and feedback technique for flight control systems of high performance aircrafts
Author
Campa, Giampiero ; Fravolini, Mario Luca ; Napolitano, Marcello R. ; Perhinschi, Mario G. ; Battipede, Manuela
Author_Institution
Dept. of Mech. & Aerosp. Eng., West Virginia Univ., Morgantown, WV, USA
Volume
2
fYear
2004
fDate
June 30 2004-July 2 2004
Firstpage
1713
Abstract
This paper focuses on a detailed description of a control technique, which has been successfully used in several advanced flight control systems research projects over the past decade. The technique, called stochastically optimal feedforward and feedback technique (SOFFT), directly descends from optimal control, and in particular from explicit model following control (EMFC). Unlike the most used model following techniques, in SOFFT the feedforward and feedback control laws are designed independently of one another. Moreover, this technique relies on different levels of plant models, specifically, a simple plant model is used for the synthesis of the feedback control law, and another plant model, together with a "command" model, are used in the synthesis of the feedforward control laws. It is important to notice that the controller in its final form is nonlinear in nature. This is because the matrices that compose the plant and command models are constantly updated as the aircraft moves throughout the flight envelope, and at least two algebraic Riccati equations (ARE) are solved in real time to compute the feedback and feedforward gains.
Keywords
Riccati equations; aircraft control; control system synthesis; digital simulation; feedback; feedforward; matrix algebra; nonlinear control systems; optimal control; stochastic systems; algebraic Riccati equations; command models; digital simulation; explicit model following control; feedback control law design; feedback control synthesis; feedback gain; feedforward control law design; feedforward control synthesis; feedforward gains; flight control systems; flight envelope; high performance aircrafts; matrix algebra; nonlinear controller; optimal control; plant models; stochastically optimal feedback technique; stochastically optimal feedforward technique;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2004. Proceedings of the 2004
Conference_Location
Boston, MA, USA
ISSN
0743-1619
Print_ISBN
0-7803-8335-4
Type
conf
Filename
1386826
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