Approximation-based Adaptive Tracking Control for 6-DoF Tailless Flying-Wing UAV with Coefficient Uncertainties
Author:
Affiliation:
1. Air Force Engineering University,Aviation Engineering School,Xi’an,China
2. Shaanxi Normal University,Xi’an,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10054511/10054645/10055837.pdf?arnumber=10055837
Reference8 articles.
1. A Robust Controller Design for a Tailless Unmanned Air Vehicle with Effective Control Allocation
2. Adaptive fault-tolerant tracking control of flying-wing unmanned aerial vehicle with system input saturation and state constraints
3. Development of a Reconfigurable Flight Control Law for Tailless Aircraft
4. Control Surface Faults Neural Adaptive Compensation Control for Tailless Flying Wing Aircraft with Uncertainties
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