A powered aircraft includes at least one thrust producing engine (20) and an engine controller (22) controllably coupled to the at least one thrust producing engine. The engine controller includes at least a first control channel (130) and a drag control channel (110). The first control channel is configured to control the at least one thrust producing engine via thrust control and the drag control channel is configured to control the at least one thrust producing engine via drag control.
DRAG CONTROL CONFIGURATION FOR A POWERED AIRCRAFT
LUFTWIDERSTANDSTEUERUNGSKONFIGURATION FÜR EIN ANGETRIEBENES FLUGZEUG
CONFIGURATION DE COMMANDE DE TRAÎNÉE DESTINÉE À UN AÉRONEF À TURBINE
2020-12-02
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Optimization of Aircraft Configuration for Minimum Drag
British Library Conference Proceedings | 2010
|Optimization of Aircraft Configuration for Minimum Drag
AIAA | 2010
|