S. V. Emel'yanov, D. A. Makarov, “Stabilization of helicopter pitch angle on various flight modes using coordinate-to-operator and operator feedbacks”, Artificial Intelligence and Decision Making, 2011, Issue 4,Pages <nobr>68

Intelligent systems and technologies

Stabilization of helicopter pitch angle on various flight modes using coordinate-to-operator and operator feedbacks

S. V. Emel'yanov^ab, D. A. Makarov^a

^a Institute for Systems Analysis of Russian Academy of Sciences
^b International Research Institute of Control Problems

Abstract: Possibility of helicopter autopilot construction based on the theory of coordinate-to-operator and operator feedback types is considered. Conclusions about stability of synthesized system under parametric uncertainty were made. Numerical simulation of various flight modes was made. Keywords: automatic control theory, helicopter control, nonlinear regulators, coordinate-to-operator feedback, operator feedback, control under uncertainty.

Keywords: automatic control theory, helicopter control, nonlinear regulators, coordinate-to-operator feedback, operator feedback, control under uncertainty.