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
2017-04-12
Patent
Electronic Resource
English