NDLI: Higher order sliding mode control applications with output redefinition for nonminimum phase missile system

Content Provider	IEEE Xplore Digital Library
Author	Parali, Y. Jafarov, E.M.
Copyright Year	2015
Description	Author affiliation: Astronaut. & Aeronaut. Dept., Istanbul Tech. Univ., Istanbul, Turkey (Jafarov, E.M.) \|\| Tactical Missile Syst. Directorate, Roketsan Missiles Inc., Ankara, Turkey (Parali, Y.)
Abstract	In this work higher order sliding mode autopilots are designed for highly maneuverable nonminimum phase missile system. Nonminimum phase nature of tail controlled missiles prevents direct implementation of sliding mode control algorithms. To overcome this difficulty an output redefinition technique is developed. Then higher order sliding mode control algorithms used for autopilot design. Second and third order SMC algorithms are tried on missile system that ideally has relative degree of two. It is showed that parasitic input-output dynamics that have lower relative degree than ideal input-output dynamics have disruptive effect on control performance. Solution is found by increasing of order of the controller and generating control signal as derivative of input. Finally adaptation schemes are applied to control algorithms to reduce chattering and increase convergence rate. Results of numerical simulation runs are given to show the effectiveness of the proposed control applications.
Starting Page	1
Ending Page	8
File Size	2496313
Page Count	8
File Format	PDF
e-ISBN	9781479989478
DOI	10.1109/RASM.2015.7154655
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2015-04-09
Publisher Place	Turkey
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Algorithm design and analysis Missiles Force Missile control Aerodynamics Higher order sliding mode control Nonminimum phase Autopilot Acceleration Adaptive control Sliding mode control Convergence
Content Type	Text
Resource Type	Article

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