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.
Helicopter control design using feedback linearization techniques
Entwurf einer Hubschrauberregelung bei Verwendung der Rückkopplungslinearisierung
1989
2 Seiten, 7 Quellen
Conference paper
English
Helicopter Motion: Equation Linearization
IEEE | 1976
|Helicopter motion: equation linearization
Tema Archive | 1976
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