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

Hardian Reza Dharmayanda, Taesam Kang, Young Jae Lee, Sangkyung Sung

Abstract


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 & 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.

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References


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DOI: http://dx.doi.org/10.21535%2FProICIUS.2007.v3.632

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