Abstract The previous Chapter presented a tracking controller of the position and heading of a helicopter based on the linearized helicopter dynamics. The adopted parametric linear model, on which the flight controller is based on, represented the quasi steady state behavior of the helicopter dynamics at hover.
Nonlinear Tracking Controller Design for Unmanned Helicopters
01.01.2011
33 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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