Helicopter control design using feedback linearization techniques

Author

Licéaga-Castro, E. ; Bradley, R. ; Castro-Linares, R.

Author_Institution

Centro de Investigacion y de Estudios Avanzados del IPN, Mexico City, Mexico

fYear

1989

fDate

13-15 Dec 1989

Firstpage

533

Abstract

Linear equivalence of nonlinear systems is applied to a helicopter model. The nonlinear control design obtained allows a transformation of the nonlinear helicopter model to a set of four linear controllable and single-input subsystems to be obtained. The main difference between the application presented and other work is that the authors express the diffeomorphic map of the state-input space in explicit form

Keywords

control system synthesis; feedback; helicopters; linearisation techniques; nonlinear control systems; control system synthesis; diffeomorphic map; feedback linearization techniques; helicopter; nonlinear control; nonlinear systems; Aerospace control; Automatic control; Control design; Cyclic redundancy check; Feedback; Helicopters; Linearization techniques;

fLanguage

English

Publisher

ieee

Conference_Titel

Decision and Control, 1989., Proceedings of the 28th IEEE Conference on

Conference_Location

Tampa, FL

Type

conf

DOI

10.1109/CDC.1989.70171

Filename

70171

Link To Document

https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3217558