Results 41 to 50 of about 1,178,972 (334)
Adaptive output feedback control of aircraft flexible modes [PDF]
, 2012 The application of adaptive output feedback augmentative control to the flexible aircraft problem is presented. Experimental validation of control scheme was carried out using a three disk torsional pendulum.
Bordeneuve-Guibé, Joël +1 more
core +1 more source
Algorithmic support of the adaptive system of controlled flight into terrain avoidance (CFITA)
Научный вестник МГТУ ГА, 2023 The article considers the restrictions algorithms for the trajectory parameters of aircraft motion. Three groups of algorithms are under consideration. They are distinguished by the volume of airborne database about terrain, modes of aircraft operation ...
A. N. Akimov +2 more
doaj +1 more source
Recent developments in the aeroelasticity of morphing aircraft
, 2021 This paper presents an extensive review of the developments in the aeroelasticity of morphing aircraft that occurred in the last decade (from 2009 to 2020).
R. Ajaj +4 more
semanticscholar +1 more source
Fracture Failure Numerical Simulation of Lug Joint Structure
Hangkong gongcheng jinzhan, 2019 Fracture of metallic materials is a difficult problem in engineering calculation. At present, researches on the ductile fracture of metal components are mostly based on the fracture samples of 10 kinds of classical plastic materials to analyze the ...
Lin Changliang, Hu Wengang, Liu Na
doaj +1 more source
A Review of Concepts, Benefits, and Challenges for Future Electrical Propulsion-Based Aircraft
Aerospace, 2020 Electrification of the propulsion system has opened the door to a new paradigm of propulsion system configurations and novel aircraft designs, which was never envisioned before.
Smruti Sahoo, Xin Zhao, K. Kyprianidis
semanticscholar +1 more source
Design and verification of skylight environment simulation system for civil aircraft
Hangkong gongcheng jinzhanThe external light environment has high impact on pilot comfort and aircraft control safety, which can affect the design of the cockpit light environment.
GUO Weihong +4 more
doaj +1 more source
Analysis on Trap Panel Structure for Aircraft Outer Wing-fuselage Connection
Hangkong gongcheng jinzhan, 2019 The trap panel structure can give full play to the role of dispersing load and reducing regional stress level. The force transfer characteristics of different types of trap panel structures are analyzed, and the main design points of trap panel ...
Tang Ping, Liu Ting, Zhang Mingxing
doaj +1 more source
Apparatus for aiding a pilot in avoiding a midair collision between aircraft [PDF]
, 1973 An apparatus for aiding a pilot in avoiding a midair collision between aircraft is described. A protected aircraft carries a transmitter, a transponder, a receiver, and a data processor; and an intruding cooperating aircraft carries a transponder.
Couch, R. H., Schrader, J. H.
core +1 more source
International Journal of Adaptive Control and Signal Processing, EarlyView.This work introduces an adaptive human pilot model that captures pilot time‐delay effects in adaptive control systems. The model enables the prediction of pilot–controller interactions, facilitating safer integration and improved design of adaptive controllers for piloted applications.
Abdullah Habboush, Yildiray Yildiz
wiley +1 more source
Xibei Gongye Daxue XuebaoAiming at the problems such as low structural bearing efficiency, structural weight gain, heavy load and cabin noise caused by high rear backbraced engine in BWB layout, based on novel materials and pultruded rod stitched efficient unitized structure ...
TIAN Rui +5 more
doaj +1 more source