Response of hang gliders to control

IF 1.4 4区工程技术 Q2 ENGINEERING, AEROSPACE

Aeronautical Journal Pub Date : 1990-10-01 DOI:10.1017/S0001924000023101

G. De Matteis

引用次数: 11

Abstract

Abstract A general dynamic model of the hang glider is applied to the analysis of response to control. The transfer functions of the glider to the longitudinal and lateral controls are formulated and some significant results, in terms of frequency response are presented and discussed. The relevant effects of the unsteady aerodynamics on the dynamics of the system are shown and the characteristics of poor lateral control are confirmed as observed in flight.

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悬挂式滑翔机对控制的响应

摘要将滑翔机的通用动力学模型应用于滑翔机的控制响应分析。推导了滑翔机对纵向和横向控制的传递函数，并给出和讨论了频率响应方面的一些重要结果。研究了非定常空气动力学对系统动力学的相关影响，并证实了飞行中观察到的横向控制不良的特征。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

Aeronautical Journal 工程技术-工程：宇航

CiteScore

3.70

自引率

14.30%

发文量

审稿时长

6-12 weeks

期刊介绍： The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.