Design/Development of Mini/Micro Air Vehicles through Modelling and Simulation: Case of an Autonomous Quadrotor

被引：3

作者：

Gupta, N. K. ^{[1
]}

Goel, R. ^{[2
]}

Ananthkrishnan, N. ^{[3
]}

机构：

[1] IDeA Res & Dev P Ltd, Pune 411013, Maharashtra, India

[2] EADS Astrium, D-88090 Friedrichshafen, Germany

[3] Korea Adv Inst Sci & Technol, Taejon 305701, South Korea

来源：

DEFENCE SCIENCE JOURNAL | 2011年 / 61卷 / 04期

关键词：

Modelling; simulation; micro air vehicle; quadrotor;

D O I：

10.14429/dsj.61.1086

中图分类号：

O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];

学科分类号：

07 ; 0710 ; 09 ;

摘要：

Design and development of an autonomous quadrotor micro aerial vehicle is undertaken following a systematic approach. A fairly detailed model was constructed and simulations were then carried out with the purpose of refining the baseline design, building a controller, and testing the flying qualities of the vehicle on a ground-based flight simulator. Following this, a smooth transition to rig and flight testing has been enabled in a cost- and time-effective manner, meeting all the design requirements.

引用

页码：337 / 345

页数：9

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