A dynamical multivariable discontinuous feedback control strategy of the sliding mode type is proposed for the altitude stabilisation of a nonlinear helicopter model in vertical flight. While retaining the basic robustness features associated with sliding mode control policies, the proposed approach also results in smoothed out (i.e. nonchattering) input trajectories and controlled state variable responses.
Dynamical sliding mode control approach for vertical flight regulation in helicopters
1994-01-01
6 pages
Article (Journal)
English
multivariable discontinuous feedback control , stability , smoothed out input trajectories , variable structure systems , vertical flight regulation , feedback , altitude stabilisation , aerospace control , helicopters , multivariable control systems , nonlinear control systems , dynamical sliding mode control , robustness features
Dynamical sliding mode control approach for vertical flight regulation in helicopters
Tema Archive | 1994
|Integrated Flight/Propulsion Control for Helicopters
British Library Conference Proceedings | 1993
|Flight Control of Airplanes and Helicopters
NTIS | 1973
|Flight simulation for helicopters
Engineering Index Backfile | 1955
Engineering Index Backfile | 1948
|