Zobrazeno 1 - 10
of 130
pro vyhledávání: '"Vijay V Patel"'
Publikováno v:
IETE Journal of Research. :1-12
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5b59b1ecc776254fa5dec0ed3afe71a2
https://doi.org/10.1080/03772063.2022.2038703
https://doi.org/10.1080/03772063.2022.2038703
Publikováno v:
Defence Science Journal. 71:153-161
The implementation of interconnect gain from aileron to rudder surface on the majority of the aircraftis to decrease sideslip which is generated because of adverse yaw with the movement of control stick in lateral axis and also enhances the turning r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::beca1c98d614888efd8afd241ecb7346
https://doi.org/10.14429/dsj.71.15347
https://doi.org/10.14429/dsj.71.15347
Publikováno v:
IFAC-PapersOnLine. 53:81-86
This paper presents autonomous landing controller design of unmanned aerial vehicles (UAVs). Feedback linearization approach with anti windup scheme is designed as autonomous landing controller. Anti windup basically controls the integrator component
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::94535a806c92a8a9147c6a664c402110
https://doi.org/10.1016/j.ifacol.2020.06.014
https://doi.org/10.1016/j.ifacol.2020.06.014
Publikováno v:
2021 International Symposium of Asian Control Association on Intelligent Robotics and Industrial Automation (IRIA).
Autonomous landing of unmanned aerial vehicle with capability to avoid reactive collision using a mixed guidance scheme, which is a combination of ‘geometric optimization technique’ and ‘collision cone approach’ has been presented in this pap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06fe59e4d48268bf67b73bc566bcf596
https://doi.org/10.1109/iria53009.2021.9588687
https://doi.org/10.1109/iria53009.2021.9588687
Publikováno v:
Intelligent Algorithms for Analysis and Control of Dynamical Systems ISBN: 9789811580444
A real-time vision-based edge detection algorithm is used for reliable fault identification and it also helps to accurately know the extent of fault. Partial loss of vertical tail of a high performance fighter aircraft is considered for this purpose.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::709efda53588bd223793da853a5fc148
https://doi.org/10.1007/978-981-15-8045-1_8
https://doi.org/10.1007/978-981-15-8045-1_8
Publikováno v:
SAE Technical Paper Series.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44c083a4ade8b2bc7875b450ef40d94f
https://doi.org/10.4271/2020-01-6003
https://doi.org/10.4271/2020-01-6003
Publikováno v:
IFAC-PapersOnLine. 51:365-370
Current fighter aircraft are demanded to feature multirole capability with large number of different external stores to be integrated on the aircraft. These stores represent air to air, air to surface weapons etc., which have wide range of aerodynami
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::12ccbd65ca9f1d18a94ddadcae4e8d10
https://doi.org/10.1016/j.ifacol.2018.05.051
https://doi.org/10.1016/j.ifacol.2018.05.051
Publikováno v:
IFAC-PapersOnLine. 51:359-364
In this paper a control topology with limited pitch and roll authority is described for automatic leveling of a fighter aircraft from disorientation. The proposed scheme provides recovery capability for an aircraft from any bank angle within the enve
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::637a27afb86dcdcef7ad3d0aa6ac459c
https://doi.org/10.1016/j.ifacol.2018.05.050
https://doi.org/10.1016/j.ifacol.2018.05.050
Publikováno v:
IFAC-PapersOnLine. 51:474-479
Auto landing of unmanned aerial vehicles with reactive collision avoidance is presented in this paper. Unmanned aerial vehicle follows approach phase, glide slope phase and flare phases during auto landing maneuver. This auto landing unmanned aerial
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::027c804881bfbba7992c1cf3baee9c71
https://doi.org/10.1016/j.ifacol.2018.05.080
https://doi.org/10.1016/j.ifacol.2018.05.080
Publikováno v:
2019 Innovations in Power and Advanced Computing Technologies (i-PACT).
Flight control engineers use certain control structure depending upon requirements and resource availability while designing flight control laws. Classical control design is carried out by assessing the stability margins of each loop while closing al
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9509f65f4bcdac464d7091e0f7e60c7c
https://doi.org/10.1109/i-pact44901.2019.8960152
https://doi.org/10.1109/i-pact44901.2019.8960152