Results 21 to 30 of about 18,209,815 (307)

The Design of General Automatic Testing Platform for Automatic Flight Control Computer

open access: yesHangkong gongcheng jinzhan, 2020
The built-in test of the aircraft can identify the fault on the automatic flight control computer when the automatic flight control computer is in failure.
HAN Jianhui, ZHANG Fen, DU Yongliang
doaj   +1 more source

Entry Guidance Command Generation for Hypersonic Glide Vehicles Under Threats and Multiple Constraints

open access: yesIEEE Access, 2022
A novel entry guidance command generation (EGCG) method for hypersonic glide vehicles (HGVs) is proposed in this paper. Apart from the conventional path constraints, terminal constraints, and multiple stationary geographic constraints, the method takes ...
Ziyao Wang, Shengjing Tang, Jie Guo
doaj   +1 more source

Research on airworthiness test technology of radiation emission in civil aircraft flight control electronic system

open access: yesXibei Gongye Daxue Xuebao, 2022
It is the first time that domestic civil large aircraft has been developed, which lacks the technical experience of airborne system-level airworthiness qualification, and the research of radiation emission at home and abroad is mainly based on simulation
LU Kuan   +4 more
doaj   +1 more source

Design and optimal control of a tiltrotor micro-aerial vehicle for efficient omnidirectional flight [PDF]

open access: yesInt. J. Robotics Res., 2020
Omnidirectional micro-aerial vehicles (MAVs) are a growing field of research, with demonstrated advantages for aerial interaction and uninhibited observation.
Mike Allenspach   +7 more
semanticscholar   +1 more source

Application of Virtualization Technology in Aeronautical Computing Field

open access: yesHangkong gongcheng jinzhan, 2022
Virtualization technology has tremendous advantages in dealing with resource allocation,application migration and isolation. To meet the demands of integration and intelligence in aeronautical computing field,as well as the constraints of real-time ...
CUI Delong, XIA Man
doaj   +1 more source

Considerations on the Development of an Electric Drive for a Secondary Flight Control Electromechanical Actuator

open access: yesIEEE transactions on industry applications, 2019
The more electric aircraft concept aims to improve the fuel consumption, the weight, and both the maintenance and operating costs of the aircraft, by promoting the use of electric power in actuation systems.
P. Giangrande   +7 more
semanticscholar   +1 more source

Learning quadrotor dynamics using neural network for flight control [PDF]

open access: yesIEEE Conference on Decision and Control, 2016
Traditional learning approaches proposed for controlling quadrotors or helicopters have focused on improving performance for specific trajectories by iteratively improving upon a nominal controller, for example learning from demonstrations, iterative ...
Somil Bansal   +4 more
semanticscholar   +1 more source

Incremental Sliding-Mode Fault-Tolerant Flight Control

open access: yesJournal of Guidance Control and Dynamics, 2019
This paper proposes a novel control framework that combines the recently reformulated incremental nonlinear dynamic inversion with (higher-order) sliding-mode controllers/observers, for generic mul...
Xuerui Wang   +3 more
semanticscholar   +1 more source

On the stabilization of leading-edge vortices with different reduced frequencies over finite-aspect-ratio pitch-up wings

open access: yesAIP Advances, 2020
An implicit large-eddy simulation method is used to numerically simulate the flowfield around a finite-span rectangular wing in pitch motion. The effect of the reduced frequency (k) on the stability of the leading-edge vortex (LEV) is studied.
JiaoLong Zhang   +3 more
doaj   +1 more source

Intelligent GNSS/INS integrated navigation system for a commercial UAV flight control system

open access: yesAerospace Science and Technology, 2018
Owing to the increase in civil applications using quadcopters, commercial flight control systems such as Pixhawk are a popular solution to provide the sensing and control functions of an unmanned aerial vehicle (UAV).
Guo-Hao Zhang, Li-Ta Hsu
semanticscholar   +1 more source

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