Attitude Control for Quadrotors Under Unknown Disturbances Using Triple-Step Method and Nonlinear Integral Sliding Mode
Author:
Affiliation:
1. School of Transportation Science and Engineering, Beihang University, Beijing, China
Funder
Defense Industrial Technology Development Program
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Electrical and Electronic Engineering,Control and Systems Engineering
Link
http://xplorestaging.ieee.org/ielx7/41/10005867/09829210.pdf?arnumber=9829210
Reference32 articles.
1. Robust cascade PID attitude control of quadrotor helicopters subject to wind disturbance
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4. A novel robust attitude control for quadrotor aircraft subject to actuator faults and wind gusts
5. Disturbance-Observer-Based Control and Related Methods—An Overview
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