학술논문

Robust regulation of helicopter model based on the highest derivative in feedback
Document Type
Conference
Source
2007 IEEE/ASME international conference on advanced intelligent mechatronics Advanced intelligent mechatronics, 2007 IEEE/ASME international conference on. :1-6 Sep, 2007
Subject
Components, Circuits, Devices and Systems
Computing and Processing
Robustness
Helicopters
Mathematical model
Feedback loop
Control systems
Aerodynamics
Control system synthesis
Laboratories
Vehicle dynamics
Sliding mode control
Language
ISSN
2159-6247
2159-6255
Abstract
The problem of robust regulation of a helicopter laboratory model is considered. The applied model has two degrees of freedom and was constructed by HUMUSOFT. This paper presents the design of continuoustime controller based on higher order output derivatives in the feedback loop. The problem of forming desired output transients for nonlinear time-varying plants under conditions of the incomplete information is discussed. The control task is formulated as a tracking problem for output variables, where decoupled output transients are accomplished in spite of incomplete information about varying parameters of the system and external disturbances. Experiments results for tracking a reference signal are presented, and confirm the effectiveness of the proposed method and theoretical expectations.