A remotely controlled VTOL aircraft includes an autopilot subsystem outputting helicopter control signals, and an autopilot subsystem outputting fixed wing control signals. A transition control subsystem is configured to receive said helicopter control signals, said fixed wing control signals, and a transition control signal. Control signals to be applied to the VTOL aircraft controls are calculated as a function of the transition percentage and weighting factors applied to the helicopter control signals and said fixed wing control signals.
REMOTELY CONTROLLED VTOL AIRCRAFT
2020-06-11
Patent
Electronic Resource
English
Remotely Controlled Modular VTOL Aircraft And Re-Configurable System Using Same
European Patent Office | 2018
|Remotely Controlled Modular VTOL Aircraft And Re-Configurable System Using Same
European Patent Office | 2020
|Remotely controlled modular VTOL aircraft and re-configurable system using same
European Patent Office | 2019
|