Zobrazeno 1 - 10
of 132
pro vyhledávání: '"Mashuq-un Nabi"'
Autor:
Shifali Kalra, Mashuq-un Nabi
Publikováno v:
The Journal of Engineering (2019)
Trajectory piecewise linear (TPWL) approximation is a well-known model order reduction technique for non-linear systems. It involves weighted summation of the dimensionally reduced linear systems obtained at certain points on the system trajectory. T
Externí odkaz:
https://doaj.org/article/e991a8f02fb644888eee31bd1b7a845f
Publikováno v:
International Journal of Robust and Nonlinear Control. 32:2845-2863
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::deb5d106b36bf2f72457b5b0147cb45f
https://doi.org/10.1002/rnc.5934
https://doi.org/10.1002/rnc.5934
Publikováno v:
IEEE Journal on Miniaturization for Air and Space Systems. 2:179-188
The controller design for a bandwidth constraint wireless control system requires a dedicated aperiodic control update strategy. In this article, an event-triggered (ET) adaptive sliding-mode control (SMC) is proposed for the attitude stabilization o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b0e14416cfc809d22bce89526ab8c7b
https://doi.org/10.1109/jmass.2021.3069938
https://doi.org/10.1109/jmass.2021.3069938
Publikováno v:
In IFAC Proceedings Volumes 2014 47(1):263-270
Publikováno v:
IET Control Theory & Applications, Vol 15, Iss 18, Pp 2286-2301 (2021)
This work proposes the use of a logarithmic quantizer to minimize the computational load on the onboard processor of missiles. The quantizer output discretizes the continuous guidance command to a finite set of predefined discrete levels. This in tur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0b6422df7bc26160e2458facb199be0a
https://doi.org/10.1049/cth2.12193
https://doi.org/10.1049/cth2.12193
Publikováno v:
IEEE Journal on Miniaturization for Air and Space Systems. 2:129-139
This article investigates the application of hysteresis quantizer for the spacecraft regulation problem under a constrained network. The hysteresis quantizer helps in quantizing the continuous control command at a lower rate of communication while av
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::93fa7ee360a56038d6680a4527013cbc
https://doi.org/10.1109/jmass.2020.3039977
https://doi.org/10.1109/jmass.2020.3039977
Publikováno v:
Journal of Dynamic Systems, Measurement, and Control. 144
This paper proposes an automatic time-energy efficient robust control (ATERC) deployment approach for selecting either a near-optimal closed-loop control law or a robust control law based on the requirement of the system. The near-optimal closed-loop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::717fab278f201b3e5a98d72bea42de52
https://doi.org/10.1115/1.4055022
https://doi.org/10.1115/1.4055022
Publikováno v:
ISA Transactions. 109:34-48
This paper proposes a time-energy efficient, artificial time delay based robust guidance strategy with input saturation for a two-dimensional interceptor problem. A reference near optimal heading trajectory is generated by applying Differential Evolu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fee6ba9c5d46d1c41a0ef7b572100519
https://doi.org/10.1016/j.isatra.2020.09.013
https://doi.org/10.1016/j.isatra.2020.09.013
Publikováno v:
Transactions of the Institute of Measurement and Control. 43:1668-1679
Active magnetic bearings (AMB) are used to suspend the rotor freely inside the stator to avoid any physical contact between them. Thus, it helps in significantly reducing the wear and tear that may cause a system breakdown. With the advancement of po
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::08b8b014e06fc56969adc351f2c04b2e
https://doi.org/10.1177/0142331220986531
https://doi.org/10.1177/0142331220986531
Publikováno v:
IEEE Journal on Miniaturization for Air and Space Systems. 1:179-187
This article presents a robust artificial time-delay-based attitude regulation control of a small spacecraft under the influence of parametric uncertainties, surrounding disturbances, and time-varying actuator faults. In the artificial time-delay (AT
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a1c2d0b0cbe31534c68b9841aaa52b66
https://doi.org/10.1109/jmass.2020.3022685
https://doi.org/10.1109/jmass.2020.3022685