DocumentCode
3586727
Title
Modeling, control and stabilization analysis on a two-link active tumbler system
Author
Sanku Niu ; Hongbin Deng ; Jie Li ; Yantao Shen
Author_Institution
Dept. of Mechatron. Eng., Beijing Inst. of Technol., Beijing, China
fYear
2014
Firstpage
211
Lastpage
216
Abstract
Tumbler system is a self-stabilized platform and its mechanical structure and premium stability properties can be used for designing coaxial helicopters without using stabilizer bar or flyer bar. The advantage of adopting a tumbler structure in coaxial helicopters is that it will replace traditional stabilizer bar or flyer bar to greatly stabilize flying attitude as well to reduce the structure complexity and volume size induced by stabilizer bars or flyer bars. In this paper, we start to study the nonlinear dynamic model of a two-link tumble system with a half circle shape at the bottom that will be extended to use in the design of a coaxial helicopter without using stabilizer bar. Based on the established model, magnitude-frequency characteristics and excited response are numerically simulated and evaluated. The PID controller is then designed for the tumbler system and dynamic responses of the controlled system are then extensively studied through simulations.
Keywords
aircraft control; control system synthesis; dynamic response; helicopters; nonlinear control systems; nonlinear dynamical systems; stability; three-term control; PID controller design; coaxial helicopter; dynamic responses; excited response; magnitude-frequency characteristics; nonlinear dynamic model; self-stabilized platform; stabilization analysis; two-link active tumbler system; Helicopters; Mathematical model; Nonlinear dynamical systems; Numerical models; Numerical stability; Servomotors; Stability analysis;
fLanguage
English
Publisher
ieee
Conference_Titel
Robotics and Biomimetics (ROBIO), 2014 IEEE International Conference on
Type
conf
DOI
10.1109/ROBIO.2014.7090332
Filename
7090332
Link To Document