Results 11 to 20 of about 25,100,536 (257)

Development of real-time flight control system for low-cost vehicle [PDF]

open access: yes, 2011
In recent years, more and more light aircraft enter our daily life, from Agricultural applications, emergency rescue, flight experiment and training to Barriers to entry, light aircraft always have their own advantages. Thus, they have become more and
Du, Yongliang
core   +7 more sources

Aerodynamic circulation control for flapless flight control of an unmanned air vehicle [PDF]

open access: yes, 2009
The supporting Flight Dynamics research contribution to the design of Demon, a flapless UAV demonstrator which is the subject of the national research programme FLAVIIR, is described in this thesis. In particular, an integrated flight control and fluidic
Buonanno, Annalisa
core   +7 more sources

Application of robust control in unmanned vehicle flight control system design [PDF]

open access: yes, 2004
The robust loop-shaping control methodology is applied in the flight control system design of the Cranfield A3 Observer unmanned, unstable, catapult launched air vehicle.
Al Swailem, Salah I.
core   +7 more sources

Development of Distributed Generic Simulator (GenSim) through Invention of Simulated Network (simNetwork) [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2011
A simulated network protocol provides the capability of distributed simulation to a generic simulator. Through this, full coverage of management of data and service handling among separated simulators is achieved. The distributed simulation environment
Cheol-Hea Koo   +2 more
doaj   +1 more source

Study on the practical method implementation of the navigation equations in a simulated FMS [PDF]

open access: yesINCAS Bulletin, 2023
This paper presents the main objective of Air Traffic Management Systems – ATMS that is to achieve optimized performance in terms of aviation safety and the enhancement of the current air transport system, through the in-depth study of the complex ...
Andrei NEAMTU   +7 more
doaj   +1 more source

Dynamic Analysis of Spatial Truss Structures Including Sliding Joint Based on the Geometrically Exact Beam Theory and Isogeometric Analysis

open access: yesApplied Sciences, 2020
With increasing of the size of spatial truss structures, the beam component will be subjected to the overall motion with large deformation. Based on the local frame approach and the geometrically exact beam theory, a beam finite element, which can ...
Zhipei Wu   +6 more
doaj   +1 more source

Extending Model-Based Systems Engineering into Integrated Platform Designed for Civil Aircraft Development [PDF]

open access: yesJournal of Aerospace Technology and Management, 2021
With the continuous development and application of modeling technology, civil aircraft designers urgently need to apply model-based systems engineering (MBSE) theory and methods into the field of civil aircraft development. However, the existing modeling
Wenhao Bi   +3 more
doaj   +2 more sources

Flight test: Supporting the investigation of factors affecting loss of control of light aircraft [PDF]

open access: yes, 2009
A quarter of all fatal General Aviation accidents in the UK during the period 1980 to 2006 involved Loss of Control (LoC) in Visual Meteorological Conditions (VMC).
Gratton, GB, Bromfield, MA
core   +6 more sources

Unfalsified Control; Application to automatic flight control system design [PDF]

open access: yesINCAS Bulletin, 2011
Unfalsified Control Theory has been developed to provide a way for avoiding modeling uncertainties in controller design. It belongs to the class of control methods called Adaptive Supervisory Switching Control, which work by introducing in the control ...
Adrian-Mihail STOICA   +1 more
doaj   +1 more source

Pre-Flight Test Verification of Automatic Stabilization System Using Aircraft Trimming Surfaces

open access: yesAerospace, 2022
The new requirement of installing the flight stabilization system onboard the airplanes for performing the single-pilot flights in IFR rules was issued lately. It caused the necessity of developing such a system for small aircraft.
Albert Zajdel   +2 more
doaj   +1 more source

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