Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Ajeet Kumar Bhatia"'
Publikováno v:
IEEE Access, Vol 7, Pp 154121-154130 (2019)
In this paper, the robust adaptive control scheme based on backstepping technique is presented that improves the trajectory tracking performance of the quadrotor unmanned aerial vehicles (UAVs), specially tasked for supply, rescue and combat missions
Externí odkaz:
https://doaj.org/article/e5ea8b7d1dee4c95933556ff25a40f3f
Publikováno v:
Engineering Computations. 39:2705-2732
PurposeBarge-type offshore floating wind turbine (OFWT) commonly exhibits an under-actuated phenomenon in an offshore environment, which leads to a potential vibration-damping hazard. This article aims to provide a new robust output feedback anti-vib
Publikováno v:
Aircraft Engineering and Aerospace Technology. 93:642-650
Purpose The purpose of this paper is to design an innovative autonomous carrier landing system (ACLS) using novel robust adaptive preview control (RAPC) method, which can assure safe and successful autonomous carrier landing under the influence of ai
Publikováno v:
International Journal of Intelligent Unmanned Systems. 10:346-362
PurposeThe aim of this research is to design a robust active disturbance attenuation control (RADAC) technique combined with an extended high gain observer (EHGO) and low pass filter (LPF).Design/methodology/approachFor designing a RADAC technique, t
Publikováno v:
Electronics Letters. 56:441-444
Before using any dataset in the intrusion detection system (IDS), it is crucial to acquire an accurate assessment of its efficiency. Nevertheless, the key complications presently met by the researchers are the deficiency of accessibility of any genui
Publikováno v:
IEEE Access, Vol 7, Pp 154121-154130 (2019)
In this paper, the robust adaptive control scheme based on backstepping technique is presented that improves the trajectory tracking performance of the quadrotor unmanned aerial vehicles (UAVs), specially tasked for supply, rescue and combat missions
Publikováno v:
Aerospace Science and Technology. 107:106244
This paper studies the tracking control problem of the air-breathing hypersonic vehicle (AHV) subject to mismatched uncertainties. A novel model transformation is proposed for AHV with uncertain parameters, to address the unavailable states problem o