Systems and methods are disclosed for coordinating and executing bidirectional energy transfer events between electrified vehicles and one or more participating electrified recreational vehicles. Energy may be transferred from an electrified vehicle to one or more electrified recreational vehicles, from the one or more electrified recreational vehicles to the electrified vehicle, or both during bidirectional energy transfer events. The proposed systems and methods may further be configured to provide various charging configurations between the electrified vehicle and the one or more electrified recreational vehicles.

A propulsion torque distribution system for a vehicle includes a controller in electronic communication with a plurality of vehicle systems. The controller executes instructions to receive at least one or more computational faults, one or more sensor faults, and a driver torque request. In response to receiving at least one of the one or more computational faults and the one or more sensor faults, the controller determines a fault that affects calculation of a primary torque request has occurred. In response to determining the fault that affects calculation of the primary torque request has occurred, the controller determines a severity of the fault. The controller determines a remedial state based on the severity of the fault. The remedial state indicates a corresponding action that is executed by the propulsion torque distribution system.

A charge coupler adapted to be coupled to a charging inlet of an electric vehicle, the charge coupler including: a housing including a first portion adapted to be disposed around a first plurality of contacts and a second portion adapted to be disposed around a second plurality of contacts; a conductive member disposed between the first portion of the housing and the second portion of the housing; and a control system coupled to the conductive member and operable for sensing a break in the conductive member indicating damage to one or more of the first portion of the housing and the second portion of the housing or that the second portion of the housing is detached from the first portion of the housing. Optionally, the conductive member includes a conductive loop disposed around an inner periphery of the housing, the first plurality of contacts, and the second plurality of contacts.

A control device for controlling a vehicle provided with a power supply function for a user includes a control unit that causes a horn of the vehicle to ring under a certain condition when a power outage is detected.

A control device for controlling a vehicle provided with a power supply function for a user includes a control unit that causes a light of the vehicle to blink under a certain condition when a power outage is detected.

A control device includes a control unit that acquires an image taken by a vehicle provided with a power supply function for a user, identifies an electric light that is turned off and that is included in the acquired image, refers to definition data that defines whether the identified electric light should be turned on during a time zone when the image was taken to determine whether a power outage has occurred.

An example method includes receiving, by one or more processors and via a sensor, a signal representing operational characteristics of a device included in an aircraft; determining, by the one or more processors and based on the signal, a partial discharge intensity value; receiving, by the one or more processors and via an environmental sensor, at least one environmental measurement of the device; modifying, by the one or more processors and based on the at least one environmental measurement, the partial discharge intensity value to determine a modified partial discharge intensity value; and responsive to determining that the modified partial discharge intensity value satisfies a threshold, outputting an alert signal for the device.

A system for mitigating charging failure for an electric aircraft including a charging connector, a sensor, a charger, and a controller. The charging connector comprising at least a charging pin and configured to mate with a corresponding charging port on an electric aircraft. The sensor communicatively connected to the charging connector and configured to detect a charging datum. The charger electrically connected to the charging connector and comprising a power source electrically connected to the charging connector. The controller communicatively connected to the sensor and configured to receive a charging datum from the sensor, detect a charging failure as a function of the charging datum, and initiate a mitigating response in response to detecting a charging failure.

A system for controlling a smart mobility by risk level includes: an information collection unit to collect position and speed information of the smart mobility and camera sensing information including a front traffic sign or object; a front detection unit to detect a front obstacle or inclination using the camera sensing information and to output a detection result; a control unit to change a warning to a user and/or a method of controlling the smart mobility by risk level based on the information collected by the information collection unit and the detection result; and a warning unit to warn the user by changing a method by risk level under the control of the control unit.

A vehicle battery charging system includes a battery charger for charging a battery module of a vehicle. A first coolant circuit conveys a first cooling fluid therethrough. The first coolant circuit includes a chiller unit separate from the vehicle. The chiller unit and the first cooling fluid exchange heat therebetween. A second coolant circuit conveys a second cooling fluid therethrough. The second coolant circuit includes a battery module. The battery module and the second cooling fluid exchange heat therebetween. A heat exchanger exchanges heat between the first cooling fluid and the second cooling fluid.