A drone flight plan between an origin and destination is evaluated with respect to planned routes of connected vehicles. The drone flight path is calculated such that it includes one or more docking segments on one or more vehicles. For multiple vehicles, multiple permutations of docking segments may be evaluated and assigned scores according to risk, drone flying time, timing issues, and other factors. A permutation having a score indicating higher desirability may be selected. The one or more vehicles may be autonomous and routes of the one or more vehicles may be adjusted in order to provide suitable docking segments for the drone flight path. The destination of the drone flight path may also be adjusted in order to permit docking on one or more vehicles.

A seismic weight dropper arrangement for a drone. The arrangement comprises a winch assembly attachable to a drone and comprising an actuator and spool with a cable windable thereon. Arrangement also includes a seismic source assembly comprising a housing and a mass suspended within the housing via at least one resiliently elastic biasing element, such as a coil spring. The seismic source assembly is fast with the cable and the actuator configured selectively to eject the seismic source assembly from the drone under the influence of gravity. The resiliently elastic biasing element has a predetermined modulus of elasticity to facilitate the mass impacting the housing when the housing impacts a surface after such ejection from a predetermined height above the surface.

The disclosed apparatus may include unmanned aerial vehicle having (1) a flight system that causes movement and hovering of the unmanned aerial vehicle, (2) a coupling mechanism that interacts with a corresponding coupling mechanism of an electronic device for carrying the electronic device from a remote location to a mount of an infrastructure component, and (3) an extension mechanism connecting the coupling mechanism to the flight system, wherein the extension mechanism dynamically extends the coupling mechanism from the flight system to facilitate installation of the electronic device to the mount while the unmanned aerial vehicle hovers. Various other apparatuses, devices, and methods are also disclosed.

A system including a landing location where a drone at least one of delivers and acquires a parcel, and a homing device to interact with the drone to guide the drone to the landing location independent of interaction from another source. The homing device guides the drone during the landing phase of a flight plan. A method is also disclosed.

An unmanned aerial vehicle (UAV) cluster includes a plurality of mission UAVs and a plurality of core UAVs arranged in a cluster. One or more of the mission UAVs is configured for controlled independent flight. The plurality of core UAVs are distributed throughout the cluster according to a selected distribution pattern that distributes the core UAVs according to a predefined mission characteristic of the UAV cluster.

Example methods and systems for coupling and controlling transport of cargo using an unmanned aerial vehicle (UAV) are provided, comprising coupling at least one electronically-controllable attachment device positioned on an underside of the UAV to a sling cable, the sling cable being secured to the cargo. The UAV flies to a predetermined area above the cargo, and responsive to determining that the UAV is positioned within the predetermined area, the UAV elevates above the initial operating height to lift the cargo and navigates to a target location.

A novel and useful system and method of air delivery of payloads incorporating a zero or near zero velocity deployment maneuver that enables aircraft to smoothly deploy payloads without dropping them and without requiring the aircraft to land. A multicopter fitted with the mechanism lowers the payload to smoothly touchdown in a matter of seconds without the need to hover above the destination. In operation, the payload hangs from a tether, pendulum, or robotic arm and is extended prior to arrival to the target destination. The hanging payload begins swinging in a controlled and coordinated manner with the trajectory of the autonomous air vehicle such that the payload arrives at the delivery point at zero or near zero velocity relative to it, while the vehicle maintains its forward movement. The payload is released from the tether at the exact moment the payload touches or is about to touch the ground.

Techniques for integrating a travel control system and attitude and heading (AHR) system in a vehicle are disclosed. The integrated system includes interface circuitry that enables data communication between constituent travel control system and AHR system of the integrated system, and can further communicate data between the travel control system and/or the AHR system and other system(s) or device(s) in or on the vehicle. In some embodiments, the travel control system includes processing circuitry that is fault tolerant. Alternatively, or additionally, the AHR system may include processing circuitry that has a processing power greater than the travel control system processing circuitry.

Embodiments described herein disclose methods and systems for community item distribution. In some implementations, the community item distribution system includes a platform for users to post information regarding items they want to share with the community. The community item distribution system can categorize the information and establish donation parameters for the shared items. The donation parameters can include where and when items can be donated or retrieved, what types of items can be donated, and who can request the donated items. In some cases, the community item distribution system can generate a user interface listing the available items that users can request. Upon request of an item, the community item distribution system can schedule a drone to transport the item, in a secured container with ultraviolet lights to disinfect the item, from the storage location to the delivery location.

A tailsitter aircraft includes an airframe, a thrust array attached to the airframe and a flight control system. The thrust array includes propulsion assemblies configured to transition the airframe from a forward flight orientation to a VTOL orientation at a conversion rate for an approach to a target ground location in a forward flight-to-VTOL transition phase. The flight control system implements an adaptive transition system including a transition parameter monitoring module configured to monitor parameters including a ground speed and a distance to the target ground location. The adaptive transition system includes a transition adjustment determination module configured to adjust the conversion rate of the airframe from the forward flight orientation to the VTOL orientation based on the ground speed and the distance to the target ground location such that the airframe is vertically aligned with the target ground location in the VTOL orientation of the forward flight-to-VTOL transition phase.