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Helicopter control design using feedback linearization techniques

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3 Author(s)
Liceaga-Castro, E. ; Centro de Investigacion y de Estudios Avanzados del IPN, Mexico City, Mexico ; Bradley, R. ; Castro-Linares, R.

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

Published in:

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

Date of Conference:

13-15 Dec 1989