Year 2017, Volume 18, Issue 4, Pages 849 - 863 2017-10-31

L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY

Ezgi ÖZÜLKÜ [1] , Hakan YAZICI [2]

168 679

In this paper a state feedback delay dependent  gain controller is designed in order to control of aircraft landing gear vibration. Based on the selection of suitable Lyapunov-Krasovskii (L-K) functional, first a Bounded Real Lemma (BRL) is obtained which enables defining stability criteria in terms of Linear Matrix Inequalities (LMIs). Extending BRL, sufficient delay-dependent criteria is developed for a stabilizing  gain controller synthesis involving a matrix inequality. Bilinear Matrix Inequality (BMI) problem is solved by utilizing cone complementary algorithm. To show the effectiveness of proposed controller on aircraft landing gear vibration, simulation studies are given. Time responses of system show that the controller guarantees stability of system with delay and has sufficient disturbance attenuation performance.   


aircraft landing gear, vibration, input delay
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Subjects Engineering
Journal Section Articles
Authors

Author: Ezgi ÖZÜLKÜ
Country: Turkey


Author: Hakan YAZICI

Dates

Publication Date: October 31, 2017

Bibtex @research article { aubtda340810, journal = {ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering}, issn = {1302-3160}, eissn = {2146-0205}, address = {Eskişehir Teknik Üniversitesi}, year = {2017}, volume = {18}, pages = {849 - 863}, doi = {10.18038/aubtda.340810}, title = {L\_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY}, key = {cite}, author = {ÖZÜLKÜ, Ezgi and YAZICI, Hakan} }
APA ÖZÜLKÜ, E , YAZICI, H . (2017). L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY. ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering, 18 (4), 849-863. Retrieved from http://dergipark.org.tr/aubtda/issue/31353/340810
MLA ÖZÜLKÜ, E , YAZICI, H . "L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY". ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering 18 (2017): 849-863 <http://dergipark.org.tr/aubtda/issue/31353/340810>
Chicago ÖZÜLKÜ, E , YAZICI, H . "L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY". ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering 18 (2017): 849-863
RIS TY - JOUR T1 - L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY AU - Ezgi ÖZÜLKÜ , Hakan YAZICI Y1 - 2017 PY - 2017 N1 - DO - T2 - ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering JF - Journal JO - JOR SP - 849 EP - 863 VL - 18 IS - 4 SN - 1302-3160-2146-0205 M3 - UR - Y2 - 2017 ER -
EndNote %0 ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY %A Ezgi ÖZÜLKÜ , Hakan YAZICI %T L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY %D 2017 %J ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering %P 1302-3160-2146-0205 %V 18 %N 4 %R %U
ISNAD ÖZÜLKÜ, Ezgi , YAZICI, Hakan . "L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY". ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering 18 / 4 (October 2017): 849-863.
AMA ÖZÜLKÜ E , YAZICI H . L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY. AUJST-A. 2017; 18(4): 849-863.
Vancouver ÖZÜLKÜ E , YAZICI H . L_2 GAIN VIBRATION CONTROL of AIRCRAFT LANDING GEAR HAVING INPUT DELAY. ANADOLU UNIVERSITY JOURNAL OF SCIENCE AND TECHNOLOGY A - Applied Sciences and Engineering. 2017; 18(4): 863-849.