Design specifications for an unmanned VTOL

被引：3

作者：

Spanoudakis, P ^{[1
]}

Tsourveloudis, NC ^{[1
]}

Valavanis, KP ^{[1
]}

机构：

[1] Tech Univ Crete, Dept Prod Engn & Management, Khania, Greece

来源：

2004 IEEE INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION, VOLS 1- 5, PROCEEDINGS | 2004年

关键词：

UAV; VTOL; design; drop test;

D O I：

10.1109/ROBOT.2004.1308813

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Parametric technology based design specifications for a new unmanned Vertical Take-Off and Landing (VTOL) vehicle are presented. The design phase is followed by performance capabilities evaluation and crash/drop tests that determine VTOL strength and frame deformations. Drop tests performed have followed standard regulations used for airworthiness certification of such vehicles. Initial drop tests have dictated a frame re-design phase that has met set VTOL specifications. The Pro\Engineer specialized Computer Aided Design (CAD) software has been used throughout all phases and tests.

引用

页码：3616 / 3621

页数：6

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