Hybrid systems model and control of a small unmanned helicopter

Author

Jianqiang, Li ; Hailong, Pei ; Xin, Liu ; Yuebang, He ; Yong, Chen

Author_Institution

Dept. of Autom., South China Univ. of Technol., Guangzhou

fYear

2008

fDate

16-18 July 2008

Firstpage

641

Lastpage

645

Abstract

To solve the optimization control problem of small unmanned helicopter nonlinear system, this paper proposes a method that models and lower-orders based on hybrid systems, obtains the maximal controlled invariant sets by states constraint, then solves the optimization problem by mixed integer quadratic programming in the sets. Finally, a model is modeled and simulated, the result proves the validity and efficiency.

Keywords

aircraft control; constraint theory; helicopters; integer programming; nonlinear control systems; quadratic programming; remotely operated vehicles; hybrid systems model; maximal controlled invariant sets; mixed integer quadratic programming; optimization control problem; states constraint; unmanned helicopter nonlinear system; Automation; Bismuth; Constraint optimization; Control system synthesis; Electronic mail; Helicopters; Helium; Modeling; Nonlinear control systems; Quadratic programming; Hybrid systems; Mix-logic dynamic model; Mixed-integer quadratic programming; Small unmanned helicopter;

fLanguage

English

Publisher

ieee

Conference_Titel

Control Conference, 2008. CCC 2008. 27th Chinese

Conference_Location

Kunming

Print_ISBN

978-7-900719-70-6

Electronic_ISBN

978-7-900719-70-6

Type

conf

DOI

10.1109/CHICC.2008.4605492

Filename

4605492