Research of Modeling and Sliding Mode Advanced Control For Four Rotor Aircraft
In the process of the design of the four rotor,control system design is a crucial link.The real thing shows a certain or strong nonlinearity.By using the classical method,the control object is simplified to the linear and small perturbation model,and then we control the small perturbation model.However,the non-linear model is controlled directly in many advanced control theories.Advanced control theory can get rid of the traditional classical control modeling of imperfection.Variable structure sliding mode adaptive control system,is a kind of advanced controller,can use the switch sliding surface makes the system achieve good stability.This article first to the four rotor model,and then designed based on sliding mode control method,and has carried on the simulation research,proved the effectiveness of the method.
Quadrotor Automatic control System Stability PID Sliding Mode Control
Zhongming Luo Xuexin Zhang Zhuofu Liu
The higher educational key laboratory for Measuring & Control Technology and Instrumentations of Heilongjiang Province Harbin University of Science and Technology Harbin, Heilongjiang, China
国际会议
秦皇岛
英文
992-996
2015-09-18（万方平台首次上网日期，不代表论文的发表时间）