DEFINING THE CONTROL LAW FOR YAW MECHANISM CONTROL OF A TRICOPTER
- 1 Aviation Faculty, National Military Universitat “Vasil Levski”, Veliko Turnovo, Bulgaria
Abstract
Behavior of a specific constructive scheme of a tricopter is modeled. On the base of real characteristics of propeller-motor system, a model of the motion of the yaw mechanism is worked out. A flight stabilization method is proposed.