A system accesses Autonomous Vehicle Communication Gateway (AVCG) information that comprises information associated with an AVCG manager. The AVCG manager is a software resource configured to transition among states in which the autonomous vehicle operates in response to detecting a respective trigger event. The system determines an autonomy status associated with the autonomous vehicle. The system detects a change in the autonomy status by accessing historical records of event, tracking back through the historical records of events, and tracking back through the AVCG information. The system determines one or more particular events from among one or both of the historical records of events and the AVCG information that led to the change in the autonomy status. The system outputs the cause of the change in the autonomy status.

A system determines that an engine of an autonomous vehicle is ignited. In response, the system transitions the autonomous vehicle into an initiation state, during which Autonomous Vehicle Communication Gateway (AVCG) configuration data is received by the autonomous vehicle. When a particular time period passes after the ignition of the engine, the system transitions the autonomous vehicle into an active state, during which instructions provided by the AVCG configuration data are executed. If the engine of the autonomous vehicle is turned off, the system transitions the autonomous vehicle into a timed-active state, during which the system sends a rescue message to an oversight server. After a timeout parameter associated with the timed-active state is reached, the system transitions the autonomous vehicle into a shutdown state, during which results of the executed instructions are stored in a local memory.

An autonomous vehicle which includes multiple independent control systems that provide redundancy as to specific and critical safety situations which may be encountered when the autonomous vehicle is in operation.

A method for flight control of an aircraft with multiple actuators during flight is disclosed. For each actuator, a control command is computed according to at least one predetermined control law and based on pilot inputs and sensor measurements in relation to a physical state of the aircraft. The respective control commands are provided to the actuators. The control commands are independently monitored by estimating or measuring a current physical state of the aircraft and comparing it with the control commands. This comparison includes checking whether the control commands stabilize the aircraft in a stable state in the absence of both disturbances and pilot inputs according to at least one predefined criterion. If the monitoring indicates a lack of stability, transmission of the control commands is prevented and a backup control command is computed for each actuator.

The automated pre-flight inspection of an unmanned aerial vehicle (UAV) uses a UAV and a dock. The UAV includes one or more cameras, one or more sub-systems, and a frame. The dock includes one or more processors, one or more memories, and one or more sensors configured for use with an automated pre-flight inspection of the UAV while the UAV is located at the dock. The one or more processors are configured to execute instructions stored in the one or more memories to perform the automated pre-flight inspection using the one or more sensors to produce output representing operational states of the one or more cameras, the one or more sub-systems, and one or more portions of the frame. The output is transmitted for display at a user device associated with the UAV.

The automated pre-flight inspection of an unmanned aerial vehicle (UAV) uses a UAV and a dock. The UAV includes one or more cameras, one or more sub-systems, and a frame. The dock includes one or more processors, one or more memories, and one or more sensors configured for use with an automated pre-flight inspection of the UAV while the UAV is located at the dock. The one or more processors are configured to execute instructions stored in the one or more memories to perform the automated pre-flight inspection using the one or more sensors to produce output representing operational states of the one or more cameras, the one or more sub-systems, and one or more portions of the frame. The output is transmitted for display at a user device associated with the UAV.

The present disclosure provides an apparatus for facilitating navigation of a device. Further, the apparatus may include a sensor board comprising two or more sensors. Further, the two or more sensors include a first sensor and a second sensor. Further, the first sensor and the second sensor may be in line on a first plane and separated by a distance. Further, the two or more sensors may be configured to generate a first sensor data and a second sensor data. Further, the apparatus may include a processing device communicatively coupled with the sensor board. Further, the processing device may be configured to analyze the first sensor data and the second sensor data. Further, the processing device may be configured to generate a navigation data. Further, the apparatus may include a communication device. Further, the communication device may be configured to transmit the navigation data to the device.

The present disclosure provides an apparatus for facilitating navigation of a device. Further, the apparatus may include a sensor board comprising two or more sensors. Further, the two or more sensors include a first sensor and a second sensor. Further, the first sensor and the second sensor may be in line on a first plane and separated by a distance. Further, the two or more sensors may be configured to generate a first sensor data and a second sensor data. Further, the apparatus may include a processing device communicatively coupled with the sensor board. Further, the processing device may be configured to analyze the first sensor data and the second sensor data. Further, the processing device may be configured to generate a navigation data. Further, the apparatus may include a communication device. Further, the communication device may be configured to transmit the navigation data to the device.

A return method and device for an aerial vehicle are provided. The method includes: during a flight process of the aerial vehicle, performing real-time planning on a return path from a current position of the aerial vehicle to a return position; performing real-time transmission of the return path to a terminal device to display the return path on a display interface. The aerial vehicle plans the return path in real-time during flight and sends it in real-time to the terminal device for display. This allows users to timely understand the planned return path of the aerial vehicle. Even in the event of a loss of connection between the aerial vehicle and the terminal device, the terminal device can display the return path based on the previously received information, thereby enhancing the safety of aerial vehicle return.

A return method and device for an aerial vehicle are provided. The method includes: during a flight process of the aerial vehicle, performing real-time planning on a return path from a current position of the aerial vehicle to a return position; performing real-time transmission of the return path to a terminal device to display the return path on a display interface. The aerial vehicle plans the return path in real-time during flight and sends it in real-time to the terminal device for display. This allows users to timely understand the planned return path of the aerial vehicle. Even in the event of a loss of connection between the aerial vehicle and the terminal device, the terminal device can display the return path based on the previously received information, thereby enhancing the safety of aerial vehicle return.