Full Attitude Control of a Quadrotor Using Fast Nonsingular Terminal Sliding Mode With Angular Velocity Planning-Reference-Cited by-同舟云学术

Full Attitude Control of a Quadrotor Using Fast Nonsingular Terminal Sliding Mode With Angular Velocity Planning

Author:

Lian Shikang¹,Meng Wei¹^ORCID,Shao Ke²^ORCID,Zheng Jinchuan³^ORCID,Zhu Shiquan¹,Li Hongyi¹^ORCID

Affiliation:

1. School of Automation, Guangdong University of Technology, Guangzhou, China

2. Tsinghua Shenzhen International Graduate School, Tsinghua University, Shenzhen, China

3. School of Software and Electrical Engineering, Swinburne University of Technology, Hawthorn, VIC, Australia

Funder

National Natural Science Foundation of China

Guangdong Introducing Innovative and Entrepreneurial Teams of Guangdong Province

Local Innovative and Research Teams Project of Guangdong Special Support Program

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering,Control and Systems Engineering

Link

Reference31 articles.

2. Nonlinear quadrocopter attitude control: Technical report;brescianini,2013

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