Design of thrust regulation law for adjustable lateral thrust and aerodynamics blended control aerocraft

Author

Zhao Yuyu ; Yang Baoqing

Author_Institution

Control & Simulation Center, Harbin Inst. of Technol., Harbin, China

fYear

2014

fDate

28-30 July 2014

Firstpage

568

Lastpage

572

Abstract

The thrust regulation law for adjustable lateral thrust and aerodynamics blended control aerocraft is proposed in this paper. Firstly, lateral jet engine configuration and thrust characteristics are given, while the constraint conditions are analyzed. Secondly, the dynamic model of thrust regulating process is established, and the cost function and constraint conditions of the optimization problem are determined. In addition, the thrust regulation law is proposed based on dynamic system method. Then, the analytical form of the regulation law is presented by analyzing thrust regulation process of different quadrants. Finally, the feasibility of the thrust regulation law is verified by the simulation results.

Keywords

aerodynamics; aircraft control; constraint theory; cost optimal control; jet engines; military aircraft; optimisation; adjustable lateral thrust; aerodynamics blended control aerocraft; constraint conditions; cost function; dynamic model; dynamic system method; jet engine configuration; optimization problem; thrust characteristics; thrust regulating process; thrust regulation law design; Aerodynamics; Cost function; Jet engines; Missiles; Simulation; Valves; adjustable lateral thrust; blended control; cost function; regulation law;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference (CCC), 2014 33rd Chinese

Conference_Location

Nanjing

Type

conf

DOI

10.1109/ChiCC.2014.6896686

Filename

6896686