Robust sliding mode speed hold control system design for full nonlinear aircraft model with parameter uncertainties: A step beyond

E. Abdulhamitbilal; E. M. Jafarov

doi:10.1109/VSS.2012.6163470

Robust sliding mode speed hold control system design for full nonlinear aircraft model with parameter uncertainties: A step beyond

E. Abdulhamitbilal^*, E. M. Jafarov

^*Corresponding author for this work

Department of Aeronautical Engineering

ISTAVIA Engineering

Research output: Contribution to journal › Conference article › peer-review

9 Citations (Scopus)

Abstract

In this paper, an aircraft speed hold flight control problem is addressed only in one loop via sliding mode control with parameter uncertainties in flight speed and altitude without any reconfiguration of control parameters. Complete nonlinear longitudinal flight dynamics model is built for a conventional aircraft for speed hold problem. Control commands are assumed to be elevator angle deflection and trust input of jet-engine/propeller. Actuator limits are calculated to determine violation limits. A design example is given to illustrate effectiveness of proposed control system with compared simulations for three different flight conditions.

Original language	English
Article number	6163470
Pages (from-to)	7-15
Number of pages	9
Journal	Proceedings of IEEE International Workshop on Variable Structure Systems
DOIs	https://doi.org/10.1109/VSS.2012.6163470
Publication status	Published - 2012
Event	2012 12th International Workshop on Variable Structure Systems, VSS 2012 - Mumbai, India Duration: 12 Jan 2012 → 14 Jan 2012

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title = "Robust sliding mode speed hold control system design for full nonlinear aircraft model with parameter uncertainties: A step beyond",

abstract = "In this paper, an aircraft speed hold flight control problem is addressed only in one loop via sliding mode control with parameter uncertainties in flight speed and altitude without any reconfiguration of control parameters. Complete nonlinear longitudinal flight dynamics model is built for a conventional aircraft for speed hold problem. Control commands are assumed to be elevator angle deflection and trust input of jet-engine/propeller. Actuator limits are calculated to determine violation limits. A design example is given to illustrate effectiveness of proposed control system with compared simulations for three different flight conditions.",

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year = "2012",

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language = "English",

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AB - In this paper, an aircraft speed hold flight control problem is addressed only in one loop via sliding mode control with parameter uncertainties in flight speed and altitude without any reconfiguration of control parameters. Complete nonlinear longitudinal flight dynamics model is built for a conventional aircraft for speed hold problem. Control commands are assumed to be elevator angle deflection and trust input of jet-engine/propeller. Actuator limits are calculated to determine violation limits. A design example is given to illustrate effectiveness of proposed control system with compared simulations for three different flight conditions.

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ER -

Robust sliding mode speed hold control system design for full nonlinear aircraft model with parameter uncertainties: A step beyond

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