Position Control of Quadcopter with First-Order Fast Nonsingular Terminal Sliding Mode Method
Author:
Affiliation:
1. Chung Yuan Christian University,Department of Electrical Engineering,Taoyuan City,Taiwan
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10325559/10325844/10326213.pdf?arnumber=10326213
Reference11 articles.
1. An adaptive recursive sliding mode attitude control for tiltrotor UAV in flight mode transition based on super-twisting extended state observer;xie,2021
2. Three-loop uncertainties compensator and sliding mode quadrotor control
3. Attitude Control of a Quadcopter Using Adaptive Control Technique;pérez,2017
4. Geometric Adaptive Controls of a Quadrotor Unmanned Aerial Vehicle With Decoupled Attitude Dynamics
5. A Unified SO(3) Approach to the Attitude Control Design for Quadrotors
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