A system for estimating flight range of an electric aircraft. The system generally includes at least a sensor and a flight controller. The at least a sensor is communicatively connected to at least a flight component. The at least a sensor is configured to detect a performance datum of the at least a flight component. The flight controller is communicatively connected to the at least a sensor. The flight controller is configured to receive the performance datum from the at least a sensor, determine an energy performance datum from the performance datum, determine a flight performance datum from the performance datum, generate a projected flight range datum as a function of the energy performance datum and the flight performance datum, and display the projected flight range datum. A method for estimating flight range of an electric aircraft is also provided.

A system for estimating flight range of an electric aircraft. The system generally includes at least a sensor and a computing device. The at least a sensor is communicatively connected to at least a flight component. The at least a sensor is configured to detect a performance datum of the at least a flight component. The computing device is communicatively connected to the at least a sensor. The computing device is configured to receive the performance datum from the at least a sensor, determine an energy performance datum from the performance datum, determine a flight performance datum from the performance datum, generate a projected flight range datum as a function of the energy performance datum and the flight performance datum, and display the projected flight range datum. A method for estimating flight range of an electric aircraft is also provided.

A drive system 20, 20′ for rotating a wheel 11, 11′ of an aircraft landing gear 10, 10′, is disclosed having a drive element 24, 24′, a motor 21, 21′ operable to rotate the drive element, and a driven gear 25, 25′ adapted to be attached to the wheel. The drive system has a drive configuration in which the drive element is capable of meshing with the driven gear to drive the driven gear, wherein the drive system further comprises a transmission error measurement apparatus 30, 40, the apparatus configured to obtain, over time, measurement data of one or more characteristics of the drive system when in the drive configuration, the measurement data providing an indication of a transmission error between a torque commanded by the motor and a resulting torque at the driven gear. An aircraft 100 and a method of providing an indication of a transmission error in a drive system is disclosed.

Provided is an information display device for a vehicle having a display control section acquiring information of the vehicle and a display section displaying an image selected by the display control section. The vehicle includes a shift lever that can select at least a parking range and a driving range, and an in displayed on the display section includes either a first vehicle image or a second vehicle that are images of the vehicle viewed from mutually different directions. On the display section, the display control section displays the first vehicle image when the shift lever selects the parking range and the second vehicle image when the shift lever selects at least the driving range.

A method includes generating movement signals indicative of sensed movement of a powered system in one or more directions and generating fluid level signals indicative of a sensed amount of fluid in the powered system. The method also includes, with one or more processors, receiving the movement signals and the fluid level signals from one or more accelerometers and a fluid level sensor, wherein the one or more processors also configured to filter at least some of the movement signals based on a speed at which the powered system operates. The method also includes, with a first antenna of the sensor assembly, wirelessly communicating one or more of the movement signals or the amount of fluid to a remote location.

Disclosed embodiments include computer-implemented methods, systems, and vehicles for determining a travel range of a vehicle. In an illustrative embodiment, a perimeter is determined indicating a travel range of a vehicle from a starting location based on the capacity of the battery system. At least one charging location is identified within the perimeter. An option is provided to generate an extended perimeter indicating an extended travel range of the vehicle travel from the starting location based on a recharge of the battery system at the at least one charging location. Map data is generated including at least one visualized travel range chosen from the perimeter and the extended perimeter.

Disclosed embodiments include systems, vehicles, and computer-implemented methods for adjusting a predictive energy consumption model for a vehicle based on actual energy consumption data collected for the vehicle. In an illustrative embodiment, a system includes a computing device including a processor and computer-readable media configured to store computer-executable instructions configured to cause the processor to: collect actual energy consumption data for a vehicle; generate an adjusted energy consumption model for the vehicle by adjusting a predictive energy consumption model responsive to the actual energy consumption data for the vehicle; and estimate a travel range of the vehicle based on available energy for the vehicle according to the adjusted energy consumption model.

A vehicle includes an electrical powertrain, a heater, at least one cooling loop, and a controller. The heater is configured to heat a vehicle cabin. The at least one cooling loop is configured to transport waste heat from at least one subcomponent of the electrical powertrain to the vehicle cabin. The controller is programmed to, in response to a command to heat the vehicle cabin and a command to operate in an economy mode, shut down the heater and operate the at least one cooling loop to transport the waste heat to the vehicle cabin. The controller is further programmed to, in response to the command to heat the vehicle cabin and an absence of the command to operate in the economy mode, operate the heater to heat the vehicle cabin.

A guide system for selecting from among a plurality of hydrogen filling stations includes a first communication device to receive information on a status of a hydrogen fuel dispenser from each of the plurality of hydrogen filling stations, respectively; a second communication device to receive a request for guidance to one of the hydrogen filling stations, from a vehicle terminal; and a controller to guide a hydrogen fuel vehicle having the vehicle terminal to a selected one of the hydrogen filling stations allowing the hydrogen fuel vehicle to occupy a hydrogen fuel dispenser having reference pressure, at a time point when the hydrogen fuel vehicle arrives, such that the hydrogen fuel vehicle is guided to the optimal hydrogen filling station to immediately fill hydrogen without standby time.

Methods, systems, and apparatus, including computer programs encoded on computer storage media, for unmanned aerial vehicle authorization and geofence envelope determination. One of the methods includes determining, by an electronic system in an Unmanned Aerial Vehicle (UAV), an estimated fuel remaining in the UAV. An estimated fuel consumption of the UAV is determined. Estimated information associated with wind affecting the UAV is determined using information obtained from sensors included in the UAV. Estimated flights times remaining for a current path, and one or more alternative flight paths, are determined using the determined estimated fuel remaining, determined estimated fuel consumption, determined information associated wind, and information describing each flight path. In response to the electronic system determining that the estimated fuel remaining, after completion of the current flight path, would be below a first threshold, an alternative flight path is selected.