대한전기학회:학술대회논문집 (Proceedings of the KIEE Conference)
- 대한전기학회 2001년도 하계학술대회 논문집 D
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- Pages.2234-2236
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- 2001
무인 비행기의 자세제어 구현
The Implementation of Attitude Control for A Radiocontrolled Airplane
- Kim, Jong-Hun (Div. of Electrical Eng. Hoseo University) ;
-
Yang, Seung-Hyun
(Div. of Electrical Eng. Hoseo University)
;
-
Lee, Seok-Won
(Div. of Electrical Eng. Hoseo University)
;
- Jung, Cha-Keun (Div. of Electrical Eng. Hoseo University)
- 발행 : 2001.07.18
초록
This paper describes an implementation of a radiocontrolled airplane attitude control. To obtain the model of motion, stabilizing and control coefficients, we derive the related paramaters from aerodynamics, propulsion, gravity, wind correction and atmosphere. In this model, after separating longitudinal axis and lateral axis, we can get longitudinal axis model and lateral axis model by using actuator and dynamic characteristics of engine. From these two models, we experiment two divided parts-linear part, and nonlinear part.
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