The Analysis of Multi-Rotor Attitude Simulator Based on Matlab-Reference-Cited by-同舟云学术

The Analysis of Multi-Rotor Attitude Simulator Based on Matlab

Published:2014-10 Issue: Volume:670-671 Page:1350-1357
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Zhao Zheng Xu¹,Han Li Long¹,Xu Qian¹

Affiliation:

1. Shijiazhuang Tiedao University

Abstract

There exist overfrequency issues of airframe vibration, instable fight conditions, inefficient airframe survivability and undeveloped cockpit’s eject-ability insides multi-rotor aircraft flights. This paper focuses on four-rotor aircraft researches via gathering inherent rotor attitudes with the inertial motion capture device. Based-on the resulting data analyses, the relations between flight attitudes and rotor performances are clearly figured out. This research also advances multi-rotor aircraft works, such as: drawing frameworks, evaluating simulations, designing control systems, and optimizing safety and stability properties.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.670-671.1350.pdf

Reference11 articles.

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