Saturation Managing for the Propulsion System and Optimal Dispatching Proposal for multi-rotor UAV

被引：0

作者：

Perez-Montenegro, C. ^{[1
]}

Lotufo, M. ^{[1
]}

Canuto, E. ^{[2
]}

Colangelo, L. ^{[1
]}

机构：

[1] Politecn Torino, Dept Control & Comp Engn DAUIN, Turin, Italy

[2] Politecn Torino, Turin, Italy

来源：

2014 IEEE/ASME INTERNATIONAL CONFERENCE ON ADVANCED INTELLIGENT MECHATRONICS (AIM) | 2014年

关键词：

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper states a methodology in order to manage the saturation of the propulsion system providing flexibility to the vehicle control unit. To reach this objective a n-copter propeller system is described and a general dispatching law without constrains is found. Furthermore, an optimal propeller problem is proposed and a possible solution using a recursive least squares method is presented.

引用

页码：452 / 457

页数：6

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