Finite Time Convergence Incremental Nonlinear Dynamic Inversion Based Attitude Control for Flying - Wing Aircraft with Actuator Faults

Wuhan Han, Shaojie Zhang. Finite Time Convergence Incremental Nonlinear Dynamic Inversion Based Attitude Control for Flying - Wing Aircraft with Actuator Faults. In CAA Symposium on Fault Detection, Supervision and Safety for Technical Processes, SAFEPROCESS 2019, Xiamen, China, July 5-7, 2019. pages 750-755, IEEE, 2019. [doi]

Abstract

Abstract is missing.