A system and method for an aircraft includes an air data system and an acoustic sensing system. The air data system includes a pitot tube positioned to sense a pitot pressure of an airflow about an exterior of the aircraft, and an angle of attack vane positioned to sense an angle of attack of the aircraft. The pitot pressure and the angle of attack are used to determine first air data parameters. The acoustic sensing system is configured to emit acoustic signals about the exterior of the aircraft and sense the acoustic signals as sensed data. The sensed data is used to determine second air data parameters.

A laser angle measuring device has a concave detection surface with a plurality of light sensors and an opaque light shield. One or more multi-axis gravity sense potentiometers determine the orientation of the laser angle measuring device, and a GPS receiver determines the location of the laser angle measuring device. The laser angle measuring device is part of a system including one or more laser emitters, each with one or more selectable laser sources. Each laser emitter may also include location and orientation measuring mechanisms.

The present invention provides a simple method and apparatus capable of accurately measuring the water depth of a field, in particular, the whole field.

SOLUTION: An ultrasonic transmitter/receiver and a drone equipped with an infrared transmitter/receiver or a microwave transmitter/receiver are allowed to fly over the field, and the distance between the ultrasonic wave surface reflection and the microwave or infrared ground reflection. Measure the water depth just below the drone from the difference in measurement. By flying the drone all over the field, the water depth of the entire field can be accurately measured. The measurement is preferably performed only while the drone is flying at a predetermined speed or higher.

An apparatus and method for performing optical caliper measurements remotely, including an unmanned aerial vehicle, a camera attached to the unmanned aerial vehicle, and an optical caliper measurement tool attached to the unmanned aerial vehicle, where the optical caliper measurement tool includes a mount, a laser source attached to the mount, and a beam splitter attached to the mount, where the laser source is configured to direct a laser beam through the beam splitter to split the laser beam into two parallel laser beams separated by a fixed distance.

A method for distance detection includes detecting a first distance value between a movable object and a target object in a target direction of the movable object, obtaining an inclination angle of the movable object at the target direction, and calculating a second distance value from the movable object to the target object based upon the inclination angle and the first distance value.

An electronic device is disclosed. The electronic device according to one embodiment comprises: a housing; a sensor for sensing a movement of the electronic device; a visible light communication (VLC) output module, disposed on one side of the housing, for outputting a VLC signal; and a processor disposed within the housing and electrically connected to the sensor and the VLC output module, wherein the processor may be configured to generate control information for controlling a movement of an unmanned aerial vehicle (UAV) on the basis of the detected movement of the electronic device, and to output the VLC signal including the control information to the UAV by using the VLC output module. Other various embodiments as understood from the specification are also possible.

An unmanned aerial vehicle (UAV) includes an aircraft body and a rotor assembly mounted on the aircraft body. The UAV also includes a barometer disposed external to the aircraft body and separated from the rotor assembly at a predetermined distance.

A UAV in which electric power is generated for an electric load from differentials in electric field strengths within a vicinity of powerlines includes: a plurality of electrodes separated and electrically insulated from one another for enabling differentials in voltage resulting from differentials in electric field strength experienced thereat; and electrical components electrically connected therewith and configurable to establish one or more electric circuits whereby voltage differentials causes a current to flow through the established electric circuit for powering an electric load. Preferably, the UAV includes a control assembly having one or more voltage-detector components configured to detect relative voltages of the electrodes; and a processor enabled to configurebased on the detected voltages and based on voltage and electric current specifications for powering the electric loadone or more of the electrical components to establish an electric circuit for powering the electric load.

A method is for detecting a blockage of a wind vane (12) of an aircraft, with the wind vane (12) including a support (20), a paddle (22) mounted rotating relative to the support (20) along an axis (A), a motor (28) able to exert a rotational torque on the paddle (22) along the axis (A), the motor (28) being connected to a processing unit (18). The method includes applying a predetermined blockage detection torque on the paddle (22) by the motor (28); measuring at least one piece of information representative of a resistance of the paddle (22) to the predetermined detection torque; and generating, via the processing unit (18), a blocking information signal, if a predetermined condition based on the representative information is verified.

Apparatus for generating electric power within vicinity of powerlines using varying electric fields and an electrical pathway to ground are disclosed. Such apparatus preferably include, for example, UAVs, charging stations, and power strips mountable to a powerline transmission tower. Methods and systems utilizing such apparatus further are disclosed. The electrical pathway to ground may include an interface that is tethered to a UAV and that is dragged along a shield wire behind the UAV as the UAV travels along the powerlines. The electrical pathway to ground alternatively may include an electrical connection to a ground of a support structure of the powerlines when the apparatus is a power strip mounted to the support structure.