Mathematical Modeling Of Gyroscope For Balancing Of Helicopter
In this paper, we present novel design of flight control for a two-degree-of-freedom helicopter. Now a days
automatic flight control is a crucial issue especially for emergency service. Automatic control features of 2-DOF helicopter
are usually approximated using LQR controller, which can be further enhanced in-terms of pole placement. The control
design consists of two control loops, one for elevation angle (Pitch) and other for rotational motion (Yaw). This paper
presents the non-linear flight control of 2-DOF helicopter using pole-placement regulator design for two input and two
output system. The model is developed and employed to approximate the non-linear control feature of 2-DOF helicopter
using Matlab software. Finally, the responses from obtained model and from real 2-DOF helicopter are compared.