Disclosed are methods, systems, and non-transitory computer-readable medium for controlling an automatic descent of a vehicle. For instance, the method may include: determining whether a descent trigger condition is present; and in response to determining the descent trigger condition is present, performing an automatic descent process. The automatic descent process may include: obtaining clearance data from an on-board system of the vehicle; generating a descent plan based on the clearance data, the descent plan including a supersonic-to-subsonic transition and/or a supersonic-descent to a target altitude; and generating actuator instructions to a control the vehicle to descend to the target altitude based on the descent plan.

To provide a structure capable of further improving safety of a device that autonomously moves in an emergency situation. Provided is a circuit including: a report unit configured to report action-allowable time information regarding an action-allowable time to a base station; and an action control unit configured to control an action of a moving object on the basis of an action instruction decided on the basis of the reported action-allowable time information and notified of by the base station and to control an action with reference to a map in which a danger level for each place is defined in an emergency situation.

The preferred embodiments relate to a method for controlling a flight movement of an aerial vehicle for landing the aerial vehicle, including: recording of first image data by means of a first camera device, which is provided on an aerial vehicle, and is configured to record an area of ground, wherein the first image data is indicative of a first sequence of first camera images. The method also includes recording of second image data by means of a second camera device, which is provided on the aerial vehicle, and is configured to record the area of ground, wherein the second image data is indicative of a second sequence of second camera images.

A flight control device 10 is device for controlling an unmanned aircraft 20, including: a region detection unit 11 that detects a flight-restricted region 30 in which flight is restricted; a distance calculation unit 12 that calculates a distance d from the flight-restricted region 30 to the unmanned aircraft 20; and a collision determination unit 13 that specifies an altitude and a speed of the unmanned aircraft 20, and determines whether the unmanned aircraft 20 lands in the flight-restricted region 30 in case of a crash, based on the altitude and the speed that have been specified and the calculated distance d.

[Object] To provide a structure capable of further improving safety of a device that autonomously moves in an emergency situation. [Solution] Provided is a circuit including: a report unit configured to report action-allowable time information regarding an action-allowable time to a base station; and an action control unit configured to control an action of a moving object on the basis of an action instruction decided on the basis of the reported action-allowable time information and notified of by the base station and to control an action with reference to a map in which a danger level for each place is defined in an emergency situation.

In an approach to ameliorating risk to an unmanned aerial vehicle, a computer retrieves valuation data corresponding to one or more components of an unmanned aerial vehicle. A computer detects a flight failure scenario of the unmanned aerial vehicle. A computer prioritizes a flight remediation pattern of the unmanned aerial vehicle. A computer identifies a feasibility of flight recovery. Based on the feasibility of the flight recovery, a computer determines flight capacity is lost. A computer retrieves risk calculation data. A computer calculates a damage risk for each of the one or more components using the risk calculation data. Based on the retrieved valuation data and the calculated damage risk, a computer ranks the damage risk for each of the one or more components. Based on the ranking, a computer modifies one or more movement factors of the unmanned aerial vehicle to alleviate damage.

The preferred embodiments relate to a method for controlling a flight movement of an aerial vehicle for landing the aerial vehicle, including: recording of first image data by means of a first camera device, which is provided on an aerial vehicle, and is configured to record an area of ground, wherein the first image data is indicative of a first sequence of first camera images. The method also includes recording of second image data by means of a second camera device, which is provided on the aerial vehicle, and is configured to record the area of ground, wherein the second image data is indicative of a second sequence of second camera images.

A method and a system for controlling an emergency descent of an aircraft. The system (1) includes a unit (2) for detecting an emergency situation, a unit (11) for calculating a usual emergency descent command, a unit (12) for calculating a limited emergency descent command, a selection unit (14) configured for selecting the usual emergency descent command or, if application conditions are met and if the limited descent command is less than said usual emergency descent command and greater than a regulation emergency descent command, selecting the limited emergency descent command, and a unit (4) for application, to the aircraft, of the selected emergency descent command.

A system (for determining one or more emergency escape paths for one or more emergencies that can occur during a flight of an aircraft) includes a control unit configured to automatically determine the one or more emergency escape paths for the one or more emergencies based on performance capabilities of the aircraft, terrain within at least a portion of an original flight path or the one or more emergency escape paths, and obstacles within at least a portion of the original flight path or the one or more emergency escape paths.

A device for automatically engaging an automated emergency descent of an aircraft. The device comprises a monitoring unit configured to automatically compare, repetitively, a current cabin altitude of the aircraft to an engagement threshold representing an altitude value, an activation unit configured to automatically engage the automated emergency descent when the current cabin altitude reaches the engagement threshold called main engagement threshold, and a unit for generating at least one engagement threshold configured at least to adapt the main engagement threshold according to the terrain, the main engagement threshold corresponding to the sum of a terrain altitude and a predetermined margin.