Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Hafiz Zeeshan Iqbal Khan"'
Nonlinear control allocation is an important part of modern nonlinear dynamic inversion based flight control systems which require highly accurate model of aircraft aerodynamics. Generally, an accurately implemented onboard model determines how well
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e57de3c70c722db5cb6990d30a685d52
http://arxiv.org/abs/2208.10411
http://arxiv.org/abs/2208.10411
Autor:
Farooq Aslam, Hafiz Zeeshan Iqbal Khan, Muhammad Farooq Haydar, Jahanzeb Rajput, Shakil Ahmed, Jamshed Riaz
Publikováno v:
2022 19th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5a4c8fe803e66934d09a97bad8dd1c04
https://doi.org/10.1109/ibcast54850.2022.9990293
https://doi.org/10.1109/ibcast54850.2022.9990293
Publikováno v:
2022 19th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::57561414aa82e0abf76105ae613f0c1b
https://doi.org/10.1109/ibcast54850.2022.9990509
https://doi.org/10.1109/ibcast54850.2022.9990509
Publikováno v:
2022 19th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::addb91b2810ae3e7804a93679e5dd18a
https://doi.org/10.1109/ibcast54850.2022.9990161
https://doi.org/10.1109/ibcast54850.2022.9990161
Autor:
Muhammad Nawaz, Shafia Rana, M. Z. Iqbal, Jawdat Alebraheem, Ahmed Elmoasry, Hafiz Zeeshan Iqbal Khan
Publikováno v:
Theoretical Foundations of Chemical Engineering. 54:664-674
An exact solution of the problem regarding influence of chemical reaction and buoyant force on the heat and mass transfer in a radiative flow due to non-coaxial rotation of a disk and fluid at infinity is derived by using Laplace transform. Flow fiel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78a0d37a0c30f43155eae9e52308cc3f
https://doi.org/10.1134/s0040579520040247
https://doi.org/10.1134/s0040579520040247
Figuring out the right airfoil is a crucial step in the preliminary stage of any aerial vehicle design, as its shape directly affects the overall aerodynamic characteristics of the aircraft or rotorcraft. Besides being a measure of performance, the a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::bb9426bf33a1ede9331005007f3bce6c
http://arxiv.org/abs/2109.12149
http://arxiv.org/abs/2109.12149
Publikováno v:
ECC
In this paper, a reconfigurable control scheme for a generalized class of multicopters is presented to overcome single or multiple rotor failures. In a multicopter, the rotor failure heavily affects its dynamics and thus its controllability. Limited
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7f1ab09dd21abe905d63b4c5afb71194
https://doi.org/10.23919/ecc51009.2020.9143731
https://doi.org/10.23919/ecc51009.2020.9143731
Publikováno v:
2020 17th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
A robust controller is specified, and the stability bounds of the uncertain closed-loop system are determined using the small gain, circle, positive real, and Popov criteria. A graphical approach is employed in order to demonstrate the ease with whic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::137a7b671dc4ff5dcdea4bca94806d33
https://doi.org/10.1109/ibcast47879.2020.9044597
https://doi.org/10.1109/ibcast47879.2020.9044597
Publikováno v:
2019 16th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
The problem of longitudinal flight control for a canard-configured combat aircraft is considered in this paper. The problem is characterized by unstable dynamics, unavailability of full state vector for the feedback, and unknown but bounded disturban
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::10dc84de1934c36b520ab7bc59655350
https://doi.org/10.1109/ibcast.2019.8667212
https://doi.org/10.1109/ibcast.2019.8667212
Publikováno v:
2019 16th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
Despite significant improvements in autonomous flight control systems, the automatic landing of a UAV still possess significant technical challenges, especially during the flare mode, which is usually considered as a crucial part of landing. Flare st
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dcb6d9364cd74a5cc1d17853c41ab24d
https://doi.org/10.1109/ibcast.2019.8666962
https://doi.org/10.1109/ibcast.2019.8666962