Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Mohsen Fathi Jegarkandi"'
Publikováno v:
Measurement + Control, Vol 58 (2025)
The probability of actuator lock, control surface damage, and thermal insulation failure on supersonic aircraft due to high speed and temperature is significant. Additionally, foldable fins are often used in missiles to increase the number of missile
Externí odkaz:
https://doaj.org/article/4779db23d31d43e98977a772d9f21fea
Autor:
A. Ashrafifar, Mohsen Fathi Jegarkandi
Publikováno v:
مهندسی مکانیک شریف, Vol 36.3, Iss 1, Pp 67-75 (2020)
In this paper, a new model-based fault detection method for an agile supersonic fligh
Externí odkaz:
https://doaj.org/article/90e52dcfb3b1482c966e36cd9c5c3c80
Publikováno v:
Journal of Aerospace Technology and Management, Vol 9, Iss 4 (2017)
Reference Governor is an important component of Active Fault Tolerant Control. One of the main reasons for using Reference Governor is to adjust/modify the reference trajectories to maintain the stability of the post-fault system, especially when a s
Externí odkaz:
https://doaj.org/article/8da442ba8c7a4916a662b2baaee99764
Publikováno v:
International Journal of Aerospace Engineering, Vol 2015 (2015)
A new method of integrated guidance and control for homing missiles with actuator fault against manoeuvring targets is proposed. Model of the integrated guidance and control system in the pitch plane with actuator fault and some uncertainty is develo
Externí odkaz:
https://doaj.org/article/80dae669be184eceb81904e2ca28067c
Publikováno v:
IEEE Transactions on Systems, Man, and Cybernetics: Systems. 52:1823-1837
This article focuses on the robust D-stabilization analysis of fractional-order control systems where each of the system and the controller may be of fractional order. The coefficients of the system are considered as complex linear functions of inter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::793d18dbd3691040f463a2f9b3084366
https://doi.org/10.1109/tsmc.2020.3037030
https://doi.org/10.1109/tsmc.2020.3037030
Publikováno v:
Transactions of the Institute of Measurement and Control. 42:1823-1833
An integrated guidance and control (IGC) is designed in this study for a surface-to-air missile considering burned or broken fin as a fault. The IGC model in the pitch plane is developed with various uncertainties in the presence of fin failure. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f0796dca711dbed7bcfe45abad3732e
https://doi.org/10.1177/0142331219897430
https://doi.org/10.1177/0142331219897430
Publikováno v:
Aerospace Science and Technology. 91:617-626
This paper presents fractional order multi-input multi-output (MIMO) controllers for the robust performance of airplane longitudinal motion. A novel necessary and sufficient criterion is offered by using the value set concept to analyze the robust pe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eef689ddedeed8a481273adda8ef8c08
https://doi.org/10.1016/j.ast.2019.06.036
https://doi.org/10.1016/j.ast.2019.06.036
Publikováno v:
IET Control Theory & Applications. 13:1039-1050
This study focuses on the robust D -stability analysis of fractional order interval systems (FOISes). The concept of interval means that the coefficients of the systems transfer functions are uncertain parameters that each adopts a value in a real in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::edc86f81525b5dc217cb840b6be647e6
https://doi.org/10.1049/iet-cta.2018.5111
https://doi.org/10.1049/iet-cta.2018.5111
Publikováno v:
Aerospace Science and Technology. 69:465-473
Reducing the burden of the remaining actuators through decreasing the performance gracefully is an important field in active fault tolerant control. According to the literature, two important points have been identified in the works considering grace
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7bcb6054058d612a9004d9f5feec022c
https://doi.org/10.1016/j.ast.2017.07.009
https://doi.org/10.1016/j.ast.2017.07.009
Publikováno v:
Aircraft Engineering and Aerospace Technology. 89:415-424
Purpose The purpose of this paper is to design an adaptive nonlinear controller for a nonlinear system of integrated guidance and control. Design/methodology/approach A nonlinear integrated guidance and control approach is applied to a homing, tail-c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b9e05d708bbf4717399a7d2af2e2e0e8
https://doi.org/10.1108/aeat-12-2014-0209
https://doi.org/10.1108/aeat-12-2014-0209