Flexible FlappingTo investigate the aerodynamic performance of a flexible flapping wing aircraft, a flapping-wing system were design and an experiment were set up to measure the unsteady aerodynamic forces of the flapping motion. The thrust formula and resistance formula described aerodynamic forces. ...
To investigate the aerodynamic performance of a flexible flapping wing aircraft, a flapping-wing system were design and an experiment were set up to measure the unsteady aerodynamic forces of the flapping motion. The thrust formula and resistance formula described aerodynamic forces. The lift and thru...
This work represents a new paradigm for the dynamics and control of maneuvering flexible aircraft. Using the system concept, the theory integrates seamlessly all the necessary material from the areas of analytical dynamics, structural dynamics, aerodynamics, and controls. It includes automatically all si...
副标题:For Rigid and Flexible Aircraft 出版年:2023 页数:643 ISBN:9781003266310 豆瓣评分 目前无人评价 评价: 写笔记 写书评 加入购书单 分享到 内容简介· ··· Flight Dynamics, Simulation, and Control of Aircraft: For Rigid and Flexible Aircraft explains the basics of non-linear aircraft dynamics...
In the present study, it is shown in its application to stabilization of anti-aircraft missile launchers. 关键词: antiaircraft system gyroscope dynamics and control gyroscope-stabilized platform DOI: 10.1016/j.jmps.2009.08.007 被引量: 12 年份: 2010 ...
Here you can find the scripts used in the book Dynamics of Flexible Aircraft by Palacios and Cesnik. Each folder correspond to a chapter in the book. The name of the script to launch the simulation can be found in the book under the relevant figures. The *.m scripts should run on any...
The use of nonlinear dynamics theory for the analysis of flying vehicles motion and the assessment of aircraft control systems is well known. In this paper the continuation and bifurcation methods are applied to flapping wings Micro Air Vehicle nonlinear control design problems. The search for the ...
Inspired by the integrated guidance and control design for endo-atmospheric aircraft, the integrated position and attitude control of spacecraft has attracted increasing attention and gradually induced a wide variety of study results in last over two dec
Differential thrust can be used for directional control on distributed electric propulsion aircraft. This paper presents an assessment of flight dynamics a
A feedback control design method is proposed based on the Lyapunov stability theory to derive the closed-loop stability conditions. The system dynamics model that includes the aircraft rigid body model, flexible cables, pulleys, springs, aerodynamic model, and servo motor control is established using...