A system for anchoring unmanned aerial vehicles to surfaces includes a landing pad configured to be installed on an agricultural machine, with the landing pad defining a landing surface. Furthermore, the system includes an unmanned aerial vehicle (UAV) configured to land on the landing surface and a top surface of a field across which the agricultural machine is traveling. The UAV, in turn, includes an anchoring device configured to engage soil within the field to anchor the UAV to the field when the UAV has landed on the top surface of the field. Additionally, the anchoring device is further configured to engage the landing pad to anchor the UAV to the landing surface when the UAV has landed on the landing pad.

A system for anchoring unmanned aerial vehicles to surfaces includes a landing pad configured to be installed on an agricultural machine, with the landing pad defining a landing surface. Furthermore, the system includes an unmanned aerial vehicle (UAV) configured to land on the landing surface and a top surface of a field across which the agricultural machine is traveling. The UAV, in turn, includes an anchoring device configured to engage soil within the field to anchor the UAV to the field when the UAV has landed on the top surface of the field. Additionally, the anchoring device is further configured to engage the landing pad to anchor the UAV to the landing surface when the UAV has landed on the landing pad.

A takeoff and landing assist apparatus for a flight vehicle with rotor blades causes the flight vehicle to take off from or be landed on a target point. The takeoff and landing assist apparatus includes a plurality of guide rods in parallel to each other, the plurality of guide rods being provided to one of the flight vehicle and the target point; and a plurality of guide rings into which the plurality of guide rods are insertable, the plurality of guide rings being provided to the other of the flight vehicle and the target point. A center-to-center distance between the plurality of guide rods and a center-to-center distance between the plurality of guide rings are set to be same.

A takeoff and landing assist apparatus for a flight vehicle with rotor blades causes the flight vehicle to take off from or be landed on a target point. The takeoff and landing assist apparatus includes a plurality of guide rods in parallel to each other, the plurality of guide rods being provided to one of the flight vehicle and the target point; and a plurality of guide rings into which the plurality of guide rods are insertable, the plurality of guide rings being provided to the other of the flight vehicle and the target point. A center-to-center distance between the plurality of guide rods and a center-to-center distance between the plurality of guide rings are set to be same.

Described herein are systems for automated docking of an unmanned aerial vehicle. For example, some systems include a landing surface configured to hold an unmanned aerial vehicle; a box configured to enclose the landing surface in a first arrangement of the dock and expose the landing surface in a second arrangement of the dock; and a retractable arm, wherein the landing surface is positioned at an end of the retractable arm and the retractable arm is configured to extend to move the landing surface outside of the box and contract to pull the landing surface inside of the box.

Described herein are systems for automated docking of an unmanned aerial vehicle. For example, some systems include an unmanned aerial vehicle including a propulsion mechanism, a battery, and a processing apparatus; and a dock including a landing surface with a funnel geometry shaped to fit a bottom surface of the unmanned aerial vehicle at a base of the funnel, wherein tapered sides of the funnel form corners at the base of the funnel, and a battery charger configured to charge the battery of the unmanned aerial vehicle while the unmanned aerial vehicle is on the landing surface, wherein conducting contacts of the battery charger are on the landing surface, positioned at the bottom of the funnel.

A multicopter landing platform includes a base portion, a bottom portion, disposed in the base portion, that accepts a protruding portion of the multicopter, and walls of the base portion that are sloped toward the bottom portion. The walls of the base portion may form a conic-shape. The multicopter landing platform may also include a GPS device that sends RTK corrections to a different GPS device on the multicopter. The multicopter landing platform may also include a beacon that guides the multicopter to cause the multicopter to contact the walls of the base station. The beacon may be disposed in the bottom portion. The beacon may provide a signal that is detected by the multicopter. The beacon may provide a light signal that is detected by a camera on the multicopter to guide the multicopter toward the base portion. A charging ring may be disposed in the bottom portion.

A multicopter landing platform includes a base portion, a bottom portion, disposed in the base portion, that accepts a protruding portion of the multicopter, and walls of the base portion that are sloped toward the bottom portion. The walls of the base portion may form a conic-shape. The multicopter landing platform may also include a GPS device that sends RTK corrections to a different GPS device on the multicopter. The multicopter landing platform may also include a beacon that guides the multicopter to cause the multicopter to contact the walls of the base station. The beacon may be disposed in the bottom portion. The beacon may provide a signal that is detected by the multicopter. The beacon may provide a light signal that is detected by a camera on the multicopter to guide the multicopter toward the base portion. A charging ring may be disposed in the bottom portion.

In response to a change in a state of at least some part of a vehicle, a control signal associated with countering the change in the state while the vehicle is in an occupant change state is generated. The control signal is sent to a rotor in the vehicle while the vehicle is in the occupant change state, wherein the control signal causes the rotor to move in a manner that is counter to the change in the state and the rotor rotates about a substantially vertical axis of rotation and enables the vehicle to perform vertical takeoffs and landings.

A power generation system includes an aircraft that includes a propulsor and a platform attached to a structure and configured to support the aircraft. The propulsor is configured to generate electrical power via a wind rotating the propulsor while the aircraft is supported by the platform. A method for using a propulsor of an aircraft to generate electrical power includes positioning the aircraft such that the aircraft is supported by a structure and generating the electrical power via a wind rotating the propulsor while the aircraft is supported by the structure.