Abstract:
Systems and methods are provided for swapping the battery on an unmanned aerial vehicle (UAV) while providing continuous power to at least one system on the UAV. The UAV may be able to identify and land on an energy provision station autonomously. The UAV may take off and/or land on the energy provision station. The UAV may communicate with the energy provision station. The energy provision station may store and charge batteries for use on a UAV. The UAV and/or the energy provision station may have a backup energy source to provide continuous power to the UAV.
Abstract:
An unmanned aerial vehicle is provided. The unmanned aerial vehicle includes: a battery; a battery residual quantity detector configured to detect a residual quantity of the battery; a communicator configured to perform communication with a rechargeable unmanned aerial vehicle used in charging or replacement of the battery; and a processor configured to control the communicator to transmit its operation information to the rechargeable unmanned aerial vehicle detected within a predetermined distance when the detected residual quantity of the battery is less than the predetermined reference quantity and control to wirelessly charge the battery by the power supplied from the rechargeable unmanned aerial vehicle to maintain an operable state of the unmanned aerial vehicle or replace the battery to a new battery provided from the rechargeable unmanned aerial vehicle when being close to the rechargeable unmanned aerial vehicle receiving the operation information.
Abstract:
Systems and methods are provided for swapping the battery on an unmanned aerial vehicle (UAV). The UAV may be able to identify and land on an energy provision station autonomously. The UAV may take off and/or land on the energy provision station. The UAV may communicate with the energy provision station. The energy provision station may store and charge batteries for use on a UAV.
Abstract:
Unmanned aerial vehicle charging systems including unmanned aerial vehicle charging stations having a light socket connector configured to be coupled to a light socket, a power circuit electrically coupled to the light socket connector, and a charging station body having one or more electrical contact regions electrically coupled to the power circuit. The one or more electrical contact regions are electrically engageable with one or more unmanned aerial vehicles.
Abstract:
According to an aspect, a distributed package transport system includes unmanned aerial vehicles (UAVs), each of which is configured to transport packages within a geographic area and along a travel route. The system also includes UAV enclosures dispersed within the geographic area. The UAV enclosures include a number of cells, each of which provides a receptacle to temporarily house a UAV. At least one of the UAV enclosures is dynamically assigned to a location within the geographic area. Each of the UAV enclosures includes a computer processor and communication network interface and, for each of the UAVs in transit, the UAV enclosures communicate information specifying an origination point, drop off point, and return point amongst each other and coordinate to define, based on locations of the UAV enclosures and capacities of the UAV enclosures, a refined travel route including a subset of the UAV enclosures to serve as hops.
Abstract:
An unmanned aerial vehicle comprising at least one rotor motor. The rotor motor is powered by a micro hybrid generation system. The micro hybrid generator system comprises a rechargeable battery configured to provide power to the at least one rotor motor, a small engine configured to generate mechanical power, a generator motor coupled to the small engine and configured to generate AC power using the mechanical power generated by the small engine, a bridge rectifier configured to convert the AC power generated by the generator motor to DC power and provide the DC power to either or both the rechargeable battery and the at least one rotor motor, and an electronic control unit configured to control a throttle of the small engine based, at least in part, on a power demand of at least one load, the at least one load including the at least one rotor motor.
Abstract:
Provided are a surveillance system and a surveillance method. The surveillance system includes a control tower configured to be coupled with and separated from a flying vehicle, and receive an image captured by the flying vehicle through a first communication network, wherein the control tower is further configured to transmit the received image to a central control station through a second communication network for analysis of the received image. The surveillance system may further include the flying vehicle and the central control station.
Abstract:
Electric aircraft, including in-flight rechargeable electric aircraft, and methods of operating electric aircraft, including methods for recharging electric aircraft in-flight, and method of deploying and retrieving secondary aircrafts.
Abstract:
A device receives a request for a flight path for a UAV to travel from a first location to a second location, and determines capability information for the UAV based on component information of the UAV. The device calculates the flight path based on the capability information, identifies multiple recharging stations located on or near the flight path, and selects a recharging station from the multiple recharging stations based on one or more factors. The device generates flight path instructions, for the flight path, that instruct the UAV to stop and recharge at the recharging station. The device provides the flight path instructions to the UAV to permit the UAV to travel from the first location to a location of the recharging station, stop and recharge at the recharging station, and travel from the location of the recharging station to the second location via the flight path.
Abstract:
A method of launching a powered unmanned aerial vehicle at an altitude of at least 13,000 m, the method comprising lifting the vehicle by attachment to a lighter-than-air carrier from a substantially ground-level location to an elevated altitude, causing the vehicle to detach from the carrier while the velocity of the vehicle relative to the carrier is substantially zero, the vehicle thereafter decreasing in altitude as it accelerates to a velocity where it is capable of preventing any further descent and can begin independent sustained flight.