Two methods of combining multiple response types into a single flexible command model are provided and include receiving a pilot stick input, generating an aircraft response to the pilot stick input that is a continuous blend of response types by including calculable time-varying coefficients set as a function of a magnitude of the pilot stick input and other aircraft states such as airspeed, imposing at least an angular acceleration command limit and using other non-linear elements to optimize the aircraft response to the pilot stick input.
FLEXIBLE COMMAND MODEL FOR AIRCRAFT CONTROL
FLEXIBLES BEFEHLSMODELL ZUR FLUGZEUGSTEUERUNG
MODÈLE DE COMMANDE FLEXIBLE D'UN AÉRONEF
06.05.2020
Patent
Elektronische Ressource
Englisch