Civil Aircraft Fault Tolerant Attitude Tracking based on Extended State Observers and Nonlinear Dynamic Inversion
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University,Shanghai,China,200240
Funder
National Natural Science Foundation of China
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
General Earth and Planetary Sciences,General Environmental Science
Link
http://xplorestaging.ieee.org/ielx7/5971804/9729156/09729152.pdf?arnumber=9729152
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2. Time-varying fault-tolerant formation tracking based cooperative control and guidance for multiple cruise missile systems under actuator failures and directed topologies
3. Cascade ADRC-based fault-tolerant control for a PVTOL aircraft with potential actuator failures
4. A novel robust attitude control for quadrotor aircraft subject to actuator faults and wind gusts
5. Robust sliding mode control with ESO for dual-control missile
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