Huang, Chenyu (College of Automation Engineering, Nanjing University of Aeronau), Zhang, Shaojie (Nanjing University of Aeronautics and Astronautics)

A Prescribed Performance Adaptive Optimal Control Scheme for Flying-Wing Aircraft

Scheduled for presentation during the Regular Session "Manned/Unmanned Aviation and Testbeds" (FrD3), Friday, September 4, 2020, 16:30−16:50, Edessa

2020 International Conference on Unmanned Aircraft Systems (ICUAS), September 1-4, 2020 (Postponed from June 9-12, 2020), Athens, Greece

This information is tentative and subject to change. Compiled on April 25, 2024

Abstract

A model-free adaptive control scheme combining the incremental control, recursive least squares identification, approximate dynamic programming algorithm and prescribed performance control theory is proposed for a kind of flying-wing aircrafts to improve dynamic performance for issue of regulation control. In this work, prescribed performance bound function is introduced to help simplify the adaptive controller design process so as to reduce dependence on human experience when designing and choosing certain parameters, at the meantime, the boundness and convergence of state are both guaranteed. Finally, the effectiveness of the presented approach is validated by several simulations.