Optimized super-twisting active disturbance rejection control based on nonlinear extended state observer for aircraft attitude stabilization

Description

FatemehSadat Yazdiniya and GholamReza Ansarifar propose a new control scheme for aircraft, in work from twenty twenty-five. A plane must hold its tilt and pitch steady despite gusts and faults. Their scheme pairs two ideas: a watcher that gauges outside pushes and faults in real time, and a sliding control law that fights them off.

The watcher feeds its gauge into the control law, which cancels much of the push. A learning method tunes the strength of the response. The pair prove the scheme stays stable on paper, in strict math terms. The aim is tighter tracking of the flight path and less drift when the air turns rough or the model falls short.

Catalog record

Source: https://europepmc.org/articles/PMC12748707