AIRCRAFT CONTROL USING FLATNESS

Philippe Martin (1)

1 CAS - Centre Automatique et Systèmes

A control law for an aircraft is presented. It is valid on the whole flight envelope and able to track any prescribed reference trajectory. The design relies on the flatness property of a simplified model globally approximating the real aircraft and the use of time scales.

Mots clés: Aircraft control; nonlinear control; flatness; perturbations

Domaines: Automatique / Robotique

Philippe Martin. AIRCRAFT CONTROL USING FLATNESS. IMACS/IEEE-SMC Multiconference CESA'96 - Symposium on Control, Optimization and Supervision, 1996, Lille, France. pp.194--199. ⟨hal-00935110⟩