DOIONLINE 
DOIONLINE Publish In |
International Journal of Electrical, Electronics and Data Communication (IJEEDC)-IJEEDC |
 Journal Home Volume Issue |
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Issue |
Volume-2,Issue-8 ( Aug, 2014 ) | |||||||||
Paper Title |
Mathematical Modeling Of Gyroscope For Balancing Of Helicopter | |||||||||
Author Name |
Kunal D. Lohar, D. K. Maghade | |||||||||
Affilition |
Instrumentation Engineering Department, Vishwakarma Institute of Technology, Pune, India | |||||||||
Pages |
67-70 | |||||||||
Abstract |
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. | |||||||||
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