A precision landing system is described for an unmanned aerial vehicle (UAV). The system may include one or more anchors configured for placement in proximity to a landing zone, a tag configured for securement to the UAV where the tag wirelessly communicates with at least three or more of the anchors. A controller may be configured to fly the UAV towards a centerline axis defined through a first airspace zone at a first altitude above the landing zone while descending towards the first altitude and then fly the UAV towards the centerline axis defined through a second airspace zone at a second altitude which is below the first altitude while descending towards the second altitude, and finally to fly the UAV towards the centerline axis defined through a third airspace zone at a third altitude which is below the second altitude while descending towards the landing zone.

A precision landing system is described for an unmanned aerial vehicle (UAV). The system may include one or more anchors configured for placement in proximity to a landing zone, a tag configured for securement to the UAV where the tag wirelessly communicates with at least three or more of the anchors. A controller may be configured to fly the UAV towards a centerline axis defined through a first airspace zone at a first altitude above the landing zone while descending towards the first altitude and then fly the UAV towards the centerline axis defined through a second airspace zone at a second altitude which is below the first altitude while descending towards the second altitude, and finally to fly the UAV towards the centerline axis defined through a third airspace zone at a third altitude which is below the second altitude while descending towards the landing zone.

A pipeline inspection system includes an unmanned aerial vehicle (UAV) operable to travel in an airspace above a pipeline configured to transport a hydrocarbon fluid. The UAV includes sensors configured to detect a leak of the hydrocarbon fluid from the pipeline. The system includes a control system configured to perform operations including operating the UAV to travel at a first altitude range in the airspace, identifying a measurement, taken at the first altitude range, from a first sensor that indicates a location of a potential leak of the hydrocarbon fluid, based on the identified measurement from the first sensor, operating the UAV to travel at a second altitude range different from the first altitude range in the airspace, identifying a measurement, taken at the second altitude range, from a second sensor that indicates the location of the potential leak, and generating a recommended action based on the identified measurements.

A pipeline inspection system includes an unmanned aerial vehicle (UAV) operable to travel in an airspace above a pipeline configured to transport a hydrocarbon fluid. The UAV includes sensors configured to detect a leak of the hydrocarbon fluid from the pipeline. The system includes a control system configured to perform operations including operating the UAV to travel at a first altitude range in the airspace, identifying a measurement, taken at the first altitude range, from a first sensor that indicates a location of a potential leak of the hydrocarbon fluid, based on the identified measurement from the first sensor, operating the UAV to travel at a second altitude range different from the first altitude range in the airspace, identifying a measurement, taken at the second altitude range, from a second sensor that indicates the location of the potential leak, and generating a recommended action based on the identified measurements.

Provided is a circuit including a report unit that reports action-allowable time information regarding an action-allowable time to a base station, and an action control unit that controls an action of a moving object on the basis of an action instruction. The action instruction is decided on the basis of the reported action-allowable time information and notified of by the base station. The action control unit further controls the action with reference to a map in which a danger level for each place is defined in an emergency situation.

A precision landing system is described for an unmanned aerial vehicle (UAV). The system may include one or more anchors configured for placement in proximity to a landing zone, a tag configured for securement to the UAV where the tag wirelessly communicates with at least three or more of the anchors. A controller may be configured to fly the UAV towards a centerline axis defined through a first airspace zone at a first altitude above the landing zone while descending towards the first altitude and then fly the UAV towards the centerline axis defined through a second airspace zone at a second altitude which is below the first altitude while descending towards the second altitude, and finally to fly the UAV towards the centerline axis defined through a third airspace zone at a third altitude which is below the second altitude while descending towards the landing zone.

A precision landing system is described for an unmanned aerial vehicle (UAV). The system may include one or more anchors configured for placement in proximity to a landing zone, a tag configured for securement to the UAV where the tag wirelessly communicates with at least three or more of the anchors. A controller may be configured to fly the UAV towards a centerline axis defined through a first airspace zone at a first altitude above the landing zone while descending towards the first altitude and then fly the UAV towards the centerline axis defined through a second airspace zone at a second altitude which is below the first altitude while descending towards the second altitude, and finally to fly the UAV towards the centerline axis defined through a third airspace zone at a third altitude which is below the second altitude while descending towards the landing zone.

The present disclosure relates generally to flight control of electric aircraft and other powered aerial vehicles. In one embodiment, a method is disclosed, comprising: receiving a descent rate command from a pilot input device, determining a proximity of each propeller of at least two propellers to a vortex ring state; and controlling the aircraft's descent rate to be less than the commanded descent rate when at least one of the at least two propellers is within a first threshold proximity to the vortex ring state.

A pipeline inspection system includes an unmanned aerial vehicle (UAV) operable to travel in an airspace above a pipeline configured to transport a hydrocarbon fluid. The UAV includes sensors configured to detect a leak of the hydrocarbon fluid from the pipeline. The system includes a control system configured to perform operations including operating the UAV to travel at a first altitude range in the airspace, identifying a measurement, taken at the first altitude range, from a first sensor that indicates a location of a potential leak of the hydrocarbon fluid, based on the identified measurement from the first sensor, operating the UAV to travel at a second altitude range different from the first altitude range in the airspace, identifying a measurement, taken at the second altitude range, from a second sensor that indicates the location of the potential leak, and generating a recommended action based on the identified measurements.

A pipeline inspection system includes an unmanned aerial vehicle (UAV) operable to travel in an airspace above a pipeline configured to transport a hydrocarbon fluid. The UAV includes sensors configured to detect a leak of the hydrocarbon fluid from the pipeline. The system includes a control system configured to perform operations including operating the UAV to travel at a first altitude range in the airspace, identifying a measurement, taken at the first altitude range, from a first sensor that indicates a location of a potential leak of the hydrocarbon fluid, based on the identified measurement from the first sensor, operating the UAV to travel at a second altitude range different from the first altitude range in the airspace, identifying a measurement, taken at the second altitude range, from a second sensor that indicates the location of the potential leak, and generating a recommended action based on the identified measurements.