Abstract: An aerial vehicle, comprising: one or more motors, one or more sensors, and a flight sub-system. The one or more sensors configured to detect data. The flight sub-system includes an attitude controller module; a rate controller module; and a compensator module. The compensator module is configured to: determine a maximum RPM of the one or more motors or a maximum torque of the one or more motors; receive a torque vector from the rate controller module; determine a rotational speed of the one or more motors to generate a desired flight orientation based upon the torque vector; and consider sensor data from the one or more sensors to adjust the rotational speed of the one or more motors.

Abstract: Safety device for igniting fuel gas discharged by the orifice of a flare stack, incorporating a pilot light whose nozzle issues into the vicinity of the orifice of the flare, said pilot light which is equipped with an ignition device is connected by a supply pipe to an auxiliary fuel gas source, said supply pipe being provided with a valve having an opening position and a closing position which are controlled by a mechanism connected by a first servo-system to the detector detecting the admission of the gas to be burned into the flare stack such that the detection of a flow of gas into said stack controls the opening position of the valve and the detection of the stoppage of this flow controls the closing position of the valve, wherein the ignition means of the pilot light comprises a refractory body located in the extension of the nozzle of the pilot light, said solid body being provided with heating means for raising it and maintaining it at a temperature of at least 800.degree. C.