Abstract:
A method for autonomously operating an unmanned aerial vehicle (UAV) that includes one or more imaging devices is provided. The imaging devices are pointed away from a direction in which the UAV is flying, and subsequently, an upcoming portion of a current flight path of the UAV is imaged, using the imaging devices. In response to the imaging, an obstacle on the current flight path is detected, and an alternate flight path is planned in response thereto. The UAV is then flown along the alternate flight path, instead of the current flight path. Other embodiments are also described.
Abstract:
A method for autonomously operating an unmanned aerial vehicle (UAV) that includes one or more imaging devices is provided. The imaging devices are pointed away from a direction in which the UAV is flying, and subsequently, an upcoming portion of a current flight path of the UAV is imaged, using the imaging devices. In response to the imaging, an obstacle on the current flight path is detected, and an alternate flight path is planned in response thereto. The UAV is then flown along the alternate flight path, instead of the current flight path. Other embodiments are also described.
Abstract:
A method for controlling an unmanned aerial vehicle (UAV) is provided. The UAV comprises at least one rotor. The method includes receiving a take-off preparatory signal; controlling a rotation speed of the at least one rotor with an idle speed rotation in response to the take-off preparatory signal; increasing the rotation speed of the at least one rotor up to a rated speed rotation under predetermined conditions.
Abstract:
An unmanned aircraft structure evaluation system includes a computer system with an input unit, a display unit, one or more processors, and one or more non-transitory computer readable medium. Image display and analysis software causes the one or more processors to generate unmanned aircraft information. The unmanned aircraft information includes flight path information configured to direct an unmanned aircraft to fly a flight path around the structure.
Abstract:
A method of emergency handling is provided for a vehicle engaged with an uninhabited aerial vehicle (UAV). The method can include collecting location information if emergency situation occurs. In emergency situations, the vehicle can determine whether an operation of uninhabited aerial vehicle (UAV) is allowed based on the location information and time information. After determining whether there is a flight space for the operation of uninhabited aerial vehicle (UAV) above a vehicle, the vehicle can transmit at least one of SOS and an emergency call into the uninhabited aerial vehicle (UAV).
Abstract:
To provide a system comprising: an unmanned aerial vehicle; and a free space location database, wherein the unmanned aerial vehicle has: a camera that is capable of 360°-image capturing on a horizontal plane; a positioning apparatus that measures a location of the unmanned aerial vehicle; a direction measuring apparatus that measures a direction of the unmanned aerial vehicle; an altitude measuring apparatus that measures an altitude of the unmanned aerial vehicle; and an information transmitting unit that transmits, to the free space location database, camera image data captured by the camera at every predetermined altitude, and the location, direction and altitude of the unmanned aerial vehicle at time of image capturing by the camera, and based on the camera image data, and the location, direction and altitude of the unmanned aerial vehicle, the free space location database corrects 3D data including terrain information to generate free space location data.
Abstract:
A payload system for an unmanned aerial vehicle (“UAV”), including a plurality of payload modules configured to attach to an underside of the UAV, wherein each payload module defines a curved surface having a plurality of mounting holes therethrough, and wherein the plurality of payload modules is interconnected to form a substantially continuous mounting surface.
Abstract:
Various types of vehicle navigation may facilitate a driver of a vehicle, including lane suggestions (e.g., a message indicating that the current route of the vehicle involves an exit from the rightmost lane of a causeway). A device may be configured to formulate lane change suggestions by detecting a current lane of the driver; comparing the travel conditions of the current lane with the travel conditions of other lanes of the causeway; and presenting a lane change suggestion of another lane presenting advantageous travel conditions as compared with the current lane. The inclusion of the current lane in the selection and formulation of lane change suggestions may improve the relevance of the suggestions (e.g., presenting lane change suggestions only if the travel condition of another lane is advantageous over the current lane, and presenting lane change suggestions relative to the current lane, e.g., “move two lanes to the left”).
Abstract:
Methods, systems, and apparatus, including computer programs encoded on computer storage media, for ground control point assignment and determination. One of the methods includes receiving information describing a flight plan for the UAV to implement, the flight plan identifying one or more waypoints associated with geographic locations assigned as ground control points. A first waypoint identified in the flight plan is traveled to, and an action to designate a surface at the associated geographic location is designated as a ground control point. Location information associated with the designated surface is stored. The stored location information is provided to an outside system for storage.
Abstract:
A remote control device for remotely controlling an unmanned apparatus and a carried object carried by the unmanned apparatus includes a remote control device attitude sensor and a microprocessor. The remote control device attitude sensor is configured to detect a remote control device spatial attitude of the remote control device and output a remote control device spatial attitude signal according to the remote control device spatial attitude. The microprocessor is configured to receive the remote control device spatial attitude signal, calculate an angle change of the remote control device in a remote control device dimension based on the remote control device spatial attitude signal, and generate a carried object control signal for controlling a movement of the carried object in a corresponding dimension based on the angle change of the remote control device. The corresponding dimension corresponds to the remote control device dimension.