Abstract:
Disclosed are transportable unmanned aerial vehicle (UAV) facilities. The facilities comprise a housing for holding a UAV, where the housing defines a landing area for the UAV. The facilities also comprise a structure for reducing wind speed across the landing area.
Abstract:
Aspects of the invention include a system for managing an agriculture plantation comprising a plantation information management server operable to send at least one electronic request to manage the agricultural plantation, the at least one electronic request comprises at least one target within the agricultural plantation; a central processor arranged in data communication with the plantation information management server to receive the electronic request to form a first dataset; the first dataset comprises data related to a size, a location and the at least one target within the agricultural plantation; an unmanned vehicle command and control server arranged in data communication with a plurality of base stations to deploy the plurality of base stations at predetermined locations within the agricultural plantation; each of the plurality of base stations arranged in data communication with at least one unmanned vehicle; the unmanned vehicle command and control server further arranged in data communication with the central processor to receive a second dataset related to at least one operation of the at least one unmanned vehicle; and a block segregator arranged to receive the first dataset as input to generate an output, the output comprises data related to the division of the agricultural plantation into a plurality of smaller areas.
Abstract:
Techniques are disclosed relating lighter-than-air aircraft. Such aircraft may be used for various purposes, such as providing network connectivity to areas that would otherwise lack such connectivity. For example, in some embodiments, a lighter-than-air aircraft according to this disclosure may include various types of antennas (directional or non-directional) for communicating with ground-based electronics or with other lighter-than-air aircraft.
Abstract:
Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain its position hovering over the landing area. The aircraft estimates a future attitude of the surface of the landing area and determines a landing time that corresponds to a desired attitude of the surface of the landing area. The unmanned aircraft executes a landing maneuver to bring the aircraft into contact with the surface of the landing area at the determined landing time.
Abstract:
An unmanned aerial vehicle (UAV) system provides for UAV deployment and remote, unattended operation with reduced logistics requirements. The system includes a launcher that can include one or more containers, or hangars, configured to house vertical take-off and landing (VTOL) UAVs. The system can further include a VTOL UAV orientation and charging module configured to mechanically position a UAV within a container and facilitate electrical mating and charging of a battery in the UAV. These operations, and others, can be performed by remote command that can initiate a series of pre-programmed steps. The UAV system can further include a power generation and storage subsystem, a security subsystem, a command and control subsystem and a communications subsystem. Command, control and communications can be provided between a remote station and the UAV.
Abstract:
An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).
Abstract:
A motor vehicle system includes a motor vehicle including an aircraft landing portion, and an actively propelled unmanned aircraft configured to be supported on the aircraft landing portion. The vehicle and aircraft are configured such that the vehicle can provide at least one of fuel and electrical energy to the aircraft while the aircraft is supported on the aircraft landing portion.
Abstract:
An un-manned airborne vehicle (UAV), for acquiring aeromagnetic data for geophysical surveying at low altitude on land or over water, comprising an extended fuselage that is adapted to hold and maintain magnetometer and a magnetic compensation magnetometer at a minimum distance from the avionics and propulsion systems of the UAV. The magnetometer measures magnetic anomalies and the magnetic compensation magnetometer measures magnetic responses corresponding to the pitch, yaw and roll of the UAV. A data acquisition system stores and removes the magnetic response measurements from the magnetic anomaly measurements. The data acquisition system also stores a survey flight plan and transmits the same to the avionics system. The generator of the UAV is shielded and the propulsion system is stabilized to reduce magnetic and vibrational noises that can interfere with the operation of the magnetometer.
Abstract:
In some embodiments, apparatuses and methods are provided herein useful to delivering merchandise using autonomous ground vehicles (AGVs) in cooperation with unmanned aerial vehicles (UAVs). In some embodiments, the system includes: an AGV having a motorized locomotion system, a storage area to hold merchandise, a sensor to detect obstacles, a transceiver, and a control circuit to operate the AGV; a UAV having a motorized flight system, a gripper mechanism to grab merchandise, a transceiver, an optical sensor to capture images; and a control circuit to operate the UAV. The system also includes a control circuit that instructs movement of the AGV along a delivery route; determines if the AGV has stopped due to an obstacle; and in certain circumstances, instructs the UAV to retrieve merchandise from the AGV, calculate a delivery route for the UAV to the delivery location, and instructs the UAV to deliver the merchandise.
Abstract:
Unmanned Aerial Vehicles also known as UAVs or Drones, either autonomous or remotely piloted, are classified as drones by the US Federal Aviation Administration (FAA) as weighing under 212 pounds. The system described herein details Autonomous Flight Vehicles (AFV) which weigh over 212 pounds but less than 1,320 pounds which may require either a new classification or a classification such as Sport Light Aircraft, but without the requirement of a pilot due to the safe autonomous flight system such as the Safe Temporal Vector Integration Engine or STeVIE. Safe Autonomous Light Aircraft (SALA) are useful as drone carriers, large scale air package or cargo transport, and even human transport depending on the total lift capability of the platform.