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Design of a robust controller for attitude stabilization of a fighter aircraft with actuator saturation

Publish place: Second Iranian Conference on Avionics System
Publish Year: 1393
Type: Conference paper
Language: English
View: 1,073

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Link to this Paper:
https://civilica.com/doc/346704

Document National Code:

ICADI02_005

Index date: 1 May 2015

Design of a robust controller for attitude stabilization of a fighter aircraft with actuator saturation abstract

This paper studies the design of a robust autopilot for a fighter aircraft by considering the actuator saturation. This goal can be achieved using CompositeNonlinear Feedback Control method (CNF) along with the Integral Sliding Mode (ISM) controller which is called ISMCNF control method. The CNF part is used to improve thetransient performance of the nominal system and the ISM part guarantees robustness against disturbances and the totalcontroller satisfies the constraint on the input in the specific region of the state space. Simulations show the effectiveperformance of the ISM-CNF method in term of robustness, andtransient response in spite of actuator saturation.

Design of a robust controller for attitude stabilization of a fighter aircraft with actuator saturation Keywords:

Actuator saturation , Composite Nonlinear Feedback (CNF) , Integral Sliding Mode (ISM)

Design of a robust controller for attitude stabilization of a fighter aircraft with actuator saturation authors

Majid Bahmani

School of Electrical and Electronic Engineering Shiraz University of Technology Modares Blvd., Shiraz, Iran

Tahereh Binazadeh

School of Electrical and Electronic Engineering Shiraz University of Technology Modares Blvd., Shiraz, Iran

Mohammad Hossein Shafiei

School of Electrical and Electronic Engineering Shiraz University of Technology Modares Blvd., Shiraz, Iran

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