Analysis of Stability, Response and LQR Controller Design of a Small Scale Helicopter Dynamics

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Apr 30, 2008
Hardian Reza Dharmayanda, Taesam Kang, Young Jae Lee, Sangkyung Sung
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This paper presents how to use feedback controller with helicopter dynamics state space model. A simplified analysis is presented for controller design using LQR of small scale helicopters for axial and forward flights. Our approach is simple and gives the basic understanding about how to develop controller for solving the stability of linear helicopter flight dynamics.

* Proceedings of the International Conference on Intelligent Unmanned System (ICIUS 2007), Bali, Indonesia, October 24-25, 2007, Paper No. ICIUS2007-C006  * Uploaded by ICIUS2007 Conference Organizer on behalf of the author(s). 8 pages, 19 figures, 4 tables  
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