A device includes hauling means for the movement of a payload while suspended from one or more lines. The or each line is suspended or suspendable from one end, the hauling means being provided at or in the region of the other end of the line/s and at which end the payload is situated in use.

The invention refers to a VTOL aircraft of the type that uses certain aerodynamic phenomena to increase the lifting force and to reduce the thrust/weight ratio. An aircraft 1 uses a propulsion system 2 consisting of four thrust producing elements, two in front 3 and two in rear 4. Each front thrust producing element 3 contains at least one front rotor 5 operated by at least one front electric motor, fixed on a fuselage 10. Each rear thrust producing element 4 contains at least one rear rotor 7 driven by at least a rear electric motor 8, fixed on the fuselage 10. On the fuselage 10 is attached symmetrically a front wing 12. On the fuselage 10 is attached symmetrically a rear wing 13. The wing 12 and 13 are used also in static conditions respectively in take-off and landing.

An aerial vehicle that comprises a main frame and a plurality of operable multicopter units. Each multicopter unit has a plurality of propulsion units. The propulsion units are attached to the respective multicopter unit at a fixed roll angle, a fixed pitch angle and a fixed yaw angle. The plurality of operable multicopter units are attached to the main frame by interposition of respective joints and rotate relative to the main frame independently to each other. At least one of the joints has a minimum of one degree of freedom, such that the main frame has a at least the same or higher number of controllable degrees of freedom than the total number of degrees of freedom of the main frame.

An integrated transportation system with vertical take-off and landing capabilities utilizes multiple common ground, pod, and flight components to facilitate efficient vertiport operations. Automated system operations, enable individuals and cargo routing between destinations in congested urban environments, as well as in remote locations selectively using the integrated ground vehicles and flight vehicles to deliver the payload pod to the destination.

An apparatus and method for centralized control of a vehicle. The apparatus includes: a processing circuitry; and a memory, the memory containing instructions that, when executed by the processing circuitry, configure the apparatus to: establish control of at least one vehicle, wherein establishing the control further comprises determining a set of instructions for controlling each vehicle; generate a mission plan for a first vehicle of the at least one vehicle based on a request from a node when the request is valid, wherein the request indicates at least a first location and a second location; send, to the first vehicle, control instructions for navigating to the first location based on the mission plan; and send, to the first vehicle, control instructions for navigating from the first location to the second location based on the mission plan, when the vehicle is at the first location.

Systems and methods for developing a three-dimensional (3D) model of a cell site using an Unmanned Aerial Vehicle (UAV) to obtain photos and/or video include preparing the UAV for flight and programming an autonomous flight path about a cell tower at the cell site, wherein the autonomous flight path comprises a substantially circular flight path about the cell tower with one or more cameras on the UAV facing the cell tower; flying the UAV around the cell tower in a plurality of orbits comprising at least four orbits each with a different set of characteristics of altitude, radius, and camera angle, wherein the flying comprises of at least four orbits for a monopole cell tower and at least five orbits for a self-support/guyed cell tower; obtaining photos and/or video of the cell tower, the cell site, and cell site components during each of the plurality of orbits; and using the photos and/or video to develop the point cloud three-dimensional (3D) model of the cell site.

In some examples, a landing location within a region for an aerial vehicle may be determined. The landing location may be determined by comparing a first digital elevation dataset and a second digital elevation dataset to identify open areas within the region. Information about the landing location can be shared with the aerial vehicle.

Systems, methods, and devices provide a vehicle, such as an aircraft, with rotors configured to function as a tri-copter for vertical takeoff and landing (VTOL) and a fixed-wing vehicle for forward flight. One rotor may be mounted at a front of the vehicle fuselage on a hinged structure controlled by an actuator to tilt from horizontal to vertical positions. Two additional rotors may be mounted on the horizontal surface of the vehicle tail structure with rotor axes oriented vertically to the fuselage. For forward flight of the vehicle, the front rotor may be rotated down such that the front rotor axis may be oriented horizontally along the fuselage and the front rotor may act as a propeller. For vertical flight, the front rotor may be rotated up such that the front rotor axis may be oriented vertically to the fuselage, while the tail rotors may be activated.

A series of convertible aircraft with a core with an airframe defining a first axis is described; a first, a second, a third, a fourth, a fifth and a sixth rotor which are rotatable about respective first, second, third, fourth, fifth and sixth axis, and operable independently of each other so as to generate respectively a first, a second, a third, a fourth, a fifth and a sixth thrust value independent of each other; the core comprises first and second portions of respective half-wings and aerodynamic surfaces and each module comprises third and fourth portions of respective half-wings and aerodynamic surfaces.

A transport system has a wheeled, steerable, self-powered, self-navigating carrier vehicle, having a substantially planar support frame, an on-board, rechargeable, battery-based power system, control circuitry, including GPS circuitry, on-board the carrier vehicle, adapted to drive and steer the carrier vehicle, and an upward-facing carrier interface adapted to the support frame, the carrier interface having first physical engagement elements, and a passenger pod adapted to carry both packages and persons, the passenger pod having a structural framework, a rechargeable, battery-based power system, and a downward-facing pod interface adapted to the structural framework, the carrier interface having second physical engagement elements. The passenger pod, placed upon the carrier vehicle, engages the downward-facing pod interface to the upward-facing carrier interface by the first and second physical engagement elements.