Aggressive maneuver oriented integrated fault-tolerant control of a 3-DOF helicopter with experimental validation
Author:
Funder
Fundamental Research Funds for the Central Universities
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference36 articles.
1. Aggressive maneuver oriented robust actuator fault estimation of a 3-DOF helicopter prototype considering measurement noises;Wang;IEEE/ASME Trans. Mechatron.,2021
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