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

> Research article (Actuators, 2020) · cited 11× · AI/ML

**Wikidata**: [openalex:W3049719119](https://www.wikidata.org/wiki/openalex:W3049719119)  
**Source**: https://4ort.xyz/entity/finite-time-convergence-incremental-nonlinear-dynamic-inversion-based-attitude-control-for-flyingwing-aircraft-with-actu