Modeling and Hovering Control of an Ducted-Fan UAV in Low Speed Crosswind-Reference-Cited by-同舟云学术

Modeling and Hovering Control of an Ducted-Fan UAV in Low Speed Crosswind

Published:2012-02 Issue: Volume:466-467 Page:1060-1064
ISSN:1662-8985
Container-title:Advanced Materials Research
language:
Short-container-title:AMR

Author:

An Hong Lei¹,Wang Jian Wen¹,Wang Jian¹,Ma Hong Xu¹

Affiliation:

1. National University of Defense Technology

Abstract

National University of Defense Technology has begun a research program to investigate and test ducted-fan propeller architecture for UAV designing. Development of a prototype continues to support ongoing research in the area of autonomous systems. In this paper, we build a nonlinear dynamic model of Ducted-Fan UAV for verifying appropriate controller behavior, and design a hierarchical controller for hovering flight of the UAV.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Link

https://www.scientific.net/AMR.466-467.1060.pdf

Reference7 articles.

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