Systems and methods for dynamic control of remotely operated vehicles may include various types of sensors to detect environment, surface, and/or friction conditions proximate a vehicle. Based on the detected environment, surface, and/or friction conditions, a maximum acceleration for safe operation of the vehicle may be determined. In addition, various dynamic control limits or ranges for the vehicle may be determined based on the maximum acceleration, and the vehicle may be controlled or instructed to operate within such dynamic limits. Moreover, various notifications, alerts, and/or feedback may be presented or output for the teleoperator at the teleoperator station in order to increase environment awareness and promote safe driving behaviors.

Systems and methods for performing high-speed geofencing in accordance with various embodiments of the invention are disclosed. One embodiment includes a robotics platform including a set of one or more motors, at least one sensor, a controller comprising a set of one or more processors, and a memory containing a controller application and a backup controller application, wherein the controller application configures the set of processors to control the robotics platform by performing the steps of receiving user commands, generating commands controlling the set of one or more motors based on the received commands. The backup controller application configures the set of processors to monitor the controller and intervene as the commands received by the controller direct the robotics platform towards a boundary by performing the steps of defining a safe set identifying positions where the robotics platform is safe, defining an invariant safe set based upon a backup set, where the invariant safe set is a subset of the safe set, and the backup set is a subset of both the invariant safe set and the safe set, receiving commands controlling the set of one or more motors to track to a desired velocity, determining if the robotic platform is approaching, and upon a determination that the robotics platform is approaching a boundary of the invariant safe set, switching control of the motors from the received commands to a combination of the received commands and backup controls generated by the backup controller application.

Embodiments relate to an aircraft control and interface system configured to adaptively control an aircraft according to different flight states by modifying one or more processing control loops. The system receives sensor data from one or more sensors of the aircraft. The system determines, from the sensor data, a component of the aircraft is compromised. The system determines the aircraft is in a degraded flight state due to the compromised component. The system operates the aircraft according to the degraded flight state, wherein operating the aircraft according to the degraded flight state includes: (a) modifying one or more processing loops based on the degraded flight state and (b) generating an actuator command by applying the degraded flight state and a signal based on an input from a vehicle control interface to the modified one or more processing loops.

Systems and methods to ensure safe driving behaviors in remote driving applications may include a vehicle having an imaging device and a teleoperator station in communication with each other via a network. For example, a safety tunnel having various safety tunnel parameters may be generated based on location data, map data, vehicle data, and/or sensor data. Remote operation of the vehicle may be monitored with respect to the safety tunnel parameters, and various visual, audio, and/or haptic alerts or feedback may be presented or emitted for the teleoperator to encourage or enforce vehicle operation within the safety tunnel parameters. Further, various autonomous remote operation programs or control routines may be initiated or instructed to ensure safe driving behaviors of the vehicle based on the safety tunnel parameters.

A system and method for protecting a rotorcraft from entering a vortex ring state, the method including monitoring a vertical speed of a rotorcraft, comparing the vertical speed to a vertical speed safety threshold, and performing vortex ring state (VRS) avoidance in response to the vertical speed exceeding the vertical speed safety threshold. The performing the VRS avoidance includes determining a power margin available from one or more engines of the rotorcraft, limiting the vertical speed of the rotorcraft in response to the power margin exceeding a threshold, and increasing a forward airspeed of the rotorcraft in response to the power margin not exceeding the threshold.

A control system for a powered lift aircraft includes a pilot input device, at least one powered lift element configured to provide powered lift support to the aircraft, and a processor. The processor is configured to receive, from the pilot input device, an input indicative of one of a powered lift enabled mode or a powered lift disabled mode and control the at least one powered lift element to operate the aircraft in a selected one of the powered lift enabled mode or the powered lift disabled mode based on the received input. When the aircraft is in the powered lift enabled mode, the at least one processor is configured to control the at least one powered lift element based on a state of the aircraft. When the aircraft is in the powered lift disabled mode, the at least one processor is configured to control the at least one powered lift element to disable powered lift.

A control system for a powered lift aircraft includes a pilot input device, at least one powered lift element configured to provide powered lift support to the aircraft, and a processor. The processor is configured to receive, from the pilot input device, an input indicative of one of a powered lift enabled mode or a powered lift disabled mode and control the at least one powered lift element to operate the aircraft in a selected one of the powered lift enabled mode or the powered lift disabled mode based on the received input. When the aircraft is in the powered lift enabled mode, the at least one processor is configured to control the at least one powered lift element based on a state of the aircraft. When the aircraft is in the powered lift disabled mode, the at least one processor is configured to control the at least one powered lift element to disable powered lift.

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.

The automatic traveling method includes: causing a sprayer 1 to travel automatically along a target route in a field; executing temporary stop processing; and executing stop reservation processing. The temporary stop processing is processing to stop the sprayer at a current position in a mode in which travel of the sprayer can be resumed in the case where a temporary stop condition is satisfied during automatic travel of the sprayer. The stop reservation processing is processing to cause the sprayer to travel and thereafter stop the sprayer in a state where the travel of the sprayer can be resumed in the case where a stop reservation condition is satisfied during the automatic travel of the sprayer.