Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Jahanzeb Rajput"'
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_________::addb91b2810ae3e7804a93679e5dd18a
https://doi.org/10.1109/ibcast54850.2022.9990161
https://doi.org/10.1109/ibcast54850.2022.9990161
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:
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
Publikováno v:
2018 15th International Bhurban Conference on Applied Sciences and Technology (IBCAST).
This paper presents a robust control scheme for an over-actuated autonomous underwater vehicle. Since the vehicle is over actuated, a control allocation method is required in conjunction with baseline control law to efficiently distribute control dem
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e28036215f25e584d6e2dc9f815e05ea
https://doi.org/10.1109/ibcast.2018.8312235
https://doi.org/10.1109/ibcast.2018.8312235
Publikováno v:
Applied Mechanics and Materials. 643:54-59
The directional stability and control is crucial for the low-speed flight of a flying-wing aircraft. The split drag-rudders are well known devices used to provide directional stability and control in a flying-wing aircraft. As opposed to conventional
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4c3bd7322bf6d4076b9394cb533d192a
https://doi.org/10.4028/www.scientific.net/amm.643.54
https://doi.org/10.4028/www.scientific.net/amm.643.54
Autor:
Zhang Weiguo, Jahanzeb Rajput
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering. 228:553-564
In this article, an overview of principle research works regarding control of nonlinear nonminimum-phase systems is presented. Key concepts of some research of fundamental importance that has been done in this area are discussed. The research is cate
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94cf34ec99fe3aef79e9ccd4a7b9b9e1
https://doi.org/10.1177/0959651814535573
https://doi.org/10.1177/0959651814535573
Publikováno v:
ASCC
A backstepping based flight control system is presented for an overactuated flying wing aircraft, where the nonlinear control allocation method based on the combination of affine mapping and redistributed pseudo inverse is used to distribute the cont
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d6845e6083a7ffe344942b3e8ec7fe7c
https://doi.org/10.1109/ascc.2015.7244649
https://doi.org/10.1109/ascc.2015.7244649