A power generation control device includes: an internal combustion engine of a vehicle; a generator driven by the internal combustion engine to generate electricity; a power storage device charged by the generator; a gear mechanism that interconnects the internal combustion engine and the generator; a detection unit for detecting vehicle information of the vehicle; a power generation controller that sets a target power generation amount of the generator based on the vehicle information and calculates a target rotational speed of the internal combustion engine and a load torque of the generator according to the target power generation amount; and a rattle suppression controller which determines whether a rattle suppression control condition of the gear mechanism is satisfied or not based on the target power generation amount and raises the target rotational speed of the internal combustion engine to a predetermined rotation number when the condition is satisfied.

A system and method of this disclosure control an on/off state of a power take-off by monitoring the power demand of a fluid power circuit that includes the power take-off and a piece of equipment connected to the power take-off. The power demand may be indicated by a pressure or temperature of a fluid power circuit, by a motion of the equipment or its hand-held controller, or by an engine torque of an engine driving the power take-off. When the equipment transitions between an off state and an on state, the controller automatically engages the power take-off. When the equipment is in the on-state for a predetermined amount of time and the power demand is at or below a predetermined threshold during the predetermined amount of timethereby indicating idle time or an inactive state of the equipmentthe controller automatically disengages the power take-off.

A vehicle includes an air-conditioning (AC) compressor, an engine, a belt-integrated starter generator (BISG), and a controller. The controller, responsive to detecting a first AC compressor engagement condition, compares a first AC torque demand that is required to engage the AC compressor with an available torque from the BISG. The controller further, responsive to the available torque being insufficient to engage the AC compressor, engages the AC compressor using the available torque from the BISG and an engine torque from the engine to compensate a torque shortfall between the AC torque demand and the available torque by retarding spark timing and increasing air intake.

A control unit (21) causes release of a lockup clutch (3a) when a speed of a vehicle reaches a first vehicle speed value (V1), which is set according to a deceleration rate of the vehicle, during deceleration running of the vehicle. Further, the control unit (21) stops regenerative power generation of an alternator (11) when the speed of the vehicle reaches a second vehicle speed value (V2), which is varied according to the deceleration rate of the vehicle, during the deceleration running of the vehicle. By this control, the stop timing of the regenerative power generation of the alternator (11) during the deceleration running is set in accordance with the deceleration rate of the vehicle whereby the vehicle achieves both of fuel consumption performance and driving performance.

A hybrid electric vehicle (HEV) and a method of supporting sound input and output for the same, the method comprising: determining whether a first condition for a sound input and output function and a second condition for an internal noise level are satisfied; determining whether operation termination of an engine is possible when the first condition and the second condition are satisfied; controlling the HEV to be driven in a first mode when the operation termination of the engine is impossible; and performing noise reduction control by changing an operating point of the engine.

A vehicle and a control method of the vehicle are disclosed. In particular, the vehicle includes: a generator; a battery; a plurality of electronic components; a power distribution apparatus to distribute power from the generator and the battery to the plurality of electronic components; and a power management apparatus to determine an electrical characteristic of each of the generator, the battery and the power distribution apparatus, and a power supply relationship between the generator, the battery and the power distribution apparatus.

An electronic control unit of a hybrid vehicle is configured to determine whether or not parking operation of the hybrid vehicle is being performed. The electronic control unit is configured to control the engine and the rotary electric machine such that starting the engine when the parking operation of the hybrid vehicle is being performed is harder than starting the engine when the parking operation of the hybrid vehicle is not being performed.

A control device of a vehicle including an engine, an auxiliary machine driven by rotation of the engine, and an engagement device selectively connecting and disconnecting a power transmission path between the engine and drive wheels comprises: a coasting control portion for selectively providing a first coasting control for allowing the vehicle to coast with the engine brought into a drive state while the power transmission path is disconnected by release of the engagement device, and a second coasting control for allowing the vehicle to coast with the engine brought into a stop state while the power transmission path is connected. If a load of the auxiliary machine is equal to or greater than a predetermined load and a vehicle speed is equal to or greater than a predetermined vehicle speed when a predetermined coasting start condition is satisfied, the coasting control portion provides the first coasting control.

A voltage controlled aircraft electric propulsion system includes an electric propulsion system. The voltage controlled aircraft electric propulsion system may include electric propulsors providing thrust for the aircraft. In hybrid systems, a gas turbine engine may also be included. The electric propulsion system may include at least one electric generator power source, at least one propulsor motor load, and at least one stored energy power source, such as a battery. The propulsor motor load may be supplied power from a power supply bus. The voltage of the power supply bus may be adjusted according to an altitude of the aircraft while maintaining a substantially constant current flow to the propulsor motor load. Due to the adjustment to lower voltages at increased altitude, insulations levels may be lower.

A vehicle includes drive wheels, an energy source having an available energy, a torque-generating device powered by the energy source to provide an input torque, a transmission configured to receive the input torque and deliver an output torque to the set of drive wheels, and a controller. The controller, as part of a programmed method, predicts consumption of the available energy along a predetermined travel route using onboard data, offboard data, and a first logic block, and also corrects the predicted energy consumption using the onboard data, offboard data, and an error correction loop between a second logic block and the first logic block. The controller also executes a control action with respect to the vehicle using the corrected energy consumption, including changing a logic state of the vehicle.