Key Parameter identification of quad-rotor aircraft system based on CIFER Algorithm

DOI

10.2991/msmee-17.2017.102How to use a DOI?

Keywords

Parameter, quad-rotor, CIFER

Abstract

Currently,there are some limitations of twxisting ways of obtaining the key parameter of quad-rotor aircrafts—mechanism analysis method and experimental method,that the first one is not adapt to varied environment and need a large amount of computation,the second one especially refers to wind tunnel test requires high cost and long operating time.This paper presented a method of combining mechanism analysis method and parameter identification to estimate the key parameters of the quad-rotor,which was easy to realize and has good performance.Firstly,the system model of the quad-rotor under the hover condition was build.Then the method based on CIFER software was used to identificate the uncertainly parameters of quad-rotor on the basis of the measured data of the 3-DOF hover simulation platform.The result showed at low frequency this method is effective and accurate in system identification of quad-rotor.

Copyright

© 2017, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Hao-ran Qi
AU  - Xiao-hui Qi
PY  - 2017/05
DA  - 2017/05
TI  - Key Parameter identification of quad-rotor aircraft system based on CIFER Algorithm
BT  - Proceedings of the 2017 2nd International Conference on Materials Science, Machinery and Energy Engineering (MSMEE 2017)
PB  - Atlantis Press
SP  - 516
EP  - 522
SN  - 2352-5401
UR  - https://doi.org/10.2991/msmee-17.2017.102
DO  - 10.2991/msmee-17.2017.102
ID  - Qi2017/05
ER  -