Transition attitude control of a tail-sitter UAV based on active disturbance rejection control architecture
Author:
Affiliation:
1. Chang’an University,School of Construction Machinery,Xi’an,China
2. Northwestern Polytechnical University,School of Aeronautics,Xi’an,China
Funder
Fundamental Research Funds for the Central Universities
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9984156/9984215/09984483.pdf?arnumber=9984483
Reference14 articles.
1. From PID to Active Disturbance Rejection Control
2. Transition characteristics for a small tail-sitter unmanned aerial vehicle
3. Scaling and Bandwidth-Parameterization Based Controller Tuning;gao;Proceedings of the American Control Conference,2003
4. Dynamic Modeling and Hardware-In-Loop Simulation for a Tail-Sitter Unmanned Aerial Vehicle in Hovering Flight
5. A novel control scheme for quadrotor UAV based upon active disturbance rejection control
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