Analysis of Stability, Response and LQR Controller Design of a Small Scale Helicopter Dynamics
نویسندگان
چکیده
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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ورودعنوان ژورنال:
- CoRR
دوره abs/0804.4757 شماره
صفحات -
تاریخ انتشار 2007