A system for controlling a flight parameter, such as velocity, associated with an airship comprises a frame (211), a support structure (212) slidably mounted to the frame and configured to provide support to an airship control and a slider output signal indicative of an offset of the support structure from a predetermined neutral position of the frame and a processor (600) communicatively connected to the frame, the support structure, and the airship control, and configured to receive the slider output signal. The processor is configured to generate a control signal for modifying the flight parameter based on the slider output signal.
Lenticular Airship and Associated Controls
Linsenförmiges Luftschiff und entsprechende Steuerungen
Dirigeable lenticulaire et commandes associées
12.04.2017
Patent
Elektronische Ressource
Englisch