Abstract: Utility vehicles include ground engaging members, a frame supported by the ground engaging members, a motor supported by the frame operably coupled to the ground engaging members, and a battery configured to provide electrical power to the motor. The battery may be removable and configured to be easily charged by outside power sources such as generators and external batteries. A charger may be configured to receive instructions to charge the battery using a specific charger operating characteristic. The vehicle may also include a variety of accessory ports configured to electrically couple to accessories that use AC or DC power.

Abstract: An system for increasing the descent rate of an aircraft may include a flight control computer, an edge control system, and a speedbrake control device. The flight control computer may be configured to compute a first setting for a leading edge device and/or a trailing edge device of an aircraft wing. The edge control system may be communicatively coupled to the flight control computer and may include an edge control device having a plurality of control device positions including a cruise position. The speedbrake control device may include a plurality of speedbrake detents including a flight detent. The edge control system may be configured to automatically command the leading edge device, the trailing edge device, or both, to a deflection angle corresponding to the first setting if the edge control device is in the cruise position and the speedbrake control device is in the flight detent.

Abstract: A system for optimizing a flap setting of an aircraft may include a flap optimizing computer configured to compute an optimum flap setting for one or more flaps of an aircraft. The system may further include a flap control system communicatively coupled to the flap optimizing computer. The flap control system may be operable to select any one of a plurality of flap settings including a designated flap setting. The flap control system may be configured to automatically command the one or more flaps from a first position to a second position corresponding to the optimum flap setting in response to the selection of one of the plurality of flap settings using the flap control system.

Abstract: An system for increasing the descent rate of an aircraft may include a flight control computer, an edge control system, and a speedbrake control device. The flight control computer may be configured to compute a first setting for a leading edge device and/or a trailing edge device of an aircraft wing. The edge control system may be communicatively coupled to the flight control computer and may include an edge control device having a plurality of control device positions including a cruise position. The speedbrake control device may include a plurality of speedbrake detents including a flight detent. The edge control system may be configured to automatically command the leading edge device, the trailing edge device, or both, to a deflection angle corresponding to the first setting if the edge control device is in the cruise position and the speedbrake control device is in the flight detent.

Abstract: A system for optimizing a flap setting of an aircraft may include a flap optimizing computer configured to compute an optimum flap setting for one or more flaps of an aircraft. The system may further include a flap control system communicatively coupled to the flap optimizing computer. The flap control system may be operable to select any one of a plurality of flap settings including a designated flap setting. The flap control system may be configured to automatically command the one or more flaps from a first position to a second position corresponding to the optimum flap setting in response to the selection of one of the plurality of flap settings using the flap control system.