DESIGN OF CONVENTIONAL UNCONVENTIONAL WINGS FOR UAV's

机译：无人机的常规和非常规机翼设计

获取原文

获取原文并翻译 | 示例

页面导航

摘要
著录项
相似文献
相关主题

摘要

The importance of UAVs for military and commercial use (e.g. reconnaissance, advance warning systems, continued surveillance) is being increasingly recognized. Based on the intended flight operation envelope, several types of conventional and unconventional UAVs are being considered. The sizes vary in wing-span from 10 cm (Micro) to 70 m (High altitude / endurance operation). Payloads vary from a few gm to 1000 kg. The vehicle mass and fight Reynolds number, Re, vary in size accordingly.rnThis paper concentrates on wing design and control design aspects of typical types of UAVs. Previously established attained thrust design methods have been used in the predictions on conventional an unconventional wings.rnSeveral ideas for future work have arisen.

机译：无人机在军事和商业用途（例如侦察，预警系统，持续监视）的重要性日益得到认可。基于预期的飞行操作范围，正在考虑几种类型的常规和非常规无人机。机翼跨度的大小从10厘米（微）到70 m（高海拔/耐力操作）不等。有效载荷从几克到1000公斤不等。飞行器的质量与雷诺数Re的大小也相应地变化。本文着重于典型无人机的机翼设计和控制设计方面。在传统的和非常规的机翼的预测中已经使用了以前建立的获得的推力设计方法。

著录项

来源
《UAVs Fifteenth international conference》|2000年|p.22.1-22.13|共13页
会议地点 Bristol(GB)
作者
R. K. Nangia; M. E. Palmer; D. I. Greenwell;
展开▼
作者单位

Consulting Engineers, Nangia Aero Research Associates, Maggs House, Queens Road, BRISTOL, BS8 1QX, UK. Tel: +44 (0)117-987 3995 Fax: +44 (0)117 987 3995;

Consulting Engineers, Nangia Aero Research Associates, Maggs House, Queens Road, BRISTOL, BS8 1QX, UK. Tel: +44 (0)117-987 3995 Fax: +44 (0)117 987 3995;

Principal Scientist Aerodynamics and Hydrodynamics Centre Defence Evaluation and Research Agency, BEDFORD, MK41 6AE, UK Tel: +44 (0)123 422 5122 Fax: +44 (0)123 422 5180;

展开▼
会议组织
原文格式 PDF
正文语种 eng
中图分类无人驾驶飞机;
关键词

相似文献

外文文献
中文文献
专利

1. VTOL UAV with the Cruise Efficiency of a Conventional Fixed-Wing UAV [J] . NASA Tech Briefs . 2018,第6期

机译：VTOL无人机具有常规固定翼无人机的巡航效率
2. Design, implementation, and verification of a low-cost terminal guidance system for small fixed-wing UAVs [J] . Yachao Yang, Chang Liu, Jie Li, Journal of Field Robotics . 2021,第5期

机译：用于小型固定翼无人机的低成本终端引导系统的设计，实施和验证
3. Introduction study of design and layout of UAVs 3D printed wings in relation to optimal lightweight and load distribution [J] . Pavol Pecho, Viliam A?altovi?, Branislav Kandera, Transportation Research Procedia . 2019,第17期

机译：无人机3D打印机翼的设计和布局与最佳轻量化和载荷分布有关的介绍研究
4. Aerodynamic Design Studies of Conventional and Unconventional Wings with Winglets [C] . R. Nangia, M. Palmer, R. Doe 24th Applied Aerodynamics Conference . 2006

机译：带有小翼的常规和非常规机翼的空气动力学设计研究
5. Real-time non-linear flight control of a fixed-wing UAV =REAL-TIME NON-LINEAR FLIGHT CONTROL OF A FIXED-WING UAV [D] . Landry, Mario. 2012

机译：固定翼UAV的实时非线性飞行控制=固定翼UAV的实时非线性飞行控制
6. Preflight Contingency Planning Approach for Fixed Wing UAVs with Engine Failure in the Presence of Winds [O] . Bulent Ayhan, Chiman Kwan, Bence Budavari, 2019

机译：有风时发动机故障的固定翼无人机的飞行前应急计划方法
7. Design and Optimization of Wing Structure for a Fixed-Wing Unmanned Aerial Vehicle (UAV) [O] . Jiawen Yu 2018

机译：固定翼无人空中飞行器机翼结构的设计与优化（UAV）

DESIGN OF CONVENTIONAL UNCONVENTIONAL WINGS FOR UAV's

摘要

著录项

相似文献

相关主题

期刊订阅