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An Improved Nonlinear Dynamic Inversion Method for Altitude and Attitude Control of Nano Quad-Rotors under Persistent Uncertainties

Chen Meili Wang Yuan

南京航空航天大学学报（英文版）2018，Vol.35Issue(3)：483-493,11.

An Improved Nonlinear Dynamic Inversion Method for Altitude and Attitude Control of Nano Quad-Rotors under Persistent Uncertainties

Chen Meili ¹Wang Yuan¹

作者信息

1. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
折叠

摘要

关键词

nonlinear dynamic inversion/extended state observer/nano quad-rotor/uncertainties rejection/altitude control/attitude control

Key words

nonlinear dynamic inversion/extended state observer/nano quad-rotor/uncertainties rejection/altitude control/attitude control

分类

航空航天

引用本文复制引用

Chen Meili,Wang Yuan..An Improved Nonlinear Dynamic Inversion Method for Altitude and Attitude Control of Nano Quad-Rotors under Persistent Uncertainties[J].南京航空航天大学学报（英文版）,2018,35(3):483-493,11.

基金项目

This work was supported by the Priority Academic Program Development of Jiangsu Higher Education Institutions (PAPD) and the Advanced Research Project of Army Equipment Development (No.301020803). （PAPD）

南京航空航天大学学报（英文版）

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ISSN：1005-1120

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