A system controls engine power by self-executing contracts with an authority. A distributed method is performed at a plurality of authority apparatus, power level lock change file servers, and engine control units. Each authority apparatus provides a policy object for each Engine Control Unit (ECU). An authority sets power levels for self-executing compliance with policy constraints. A power level lock change file (LockChangeFile) server checks against date time constraints and geo-location scope by its authorities. An ECU receives a power level token when time and location constraint(s) by at least one authority is within scope. A distributed method includes receiving space time constraints and determining a policy object and Authoritative LockChangeFile; receiving date, time, and location indicia from an ECU; determining the lowest power level consistent with the LockChangeFile; and requesting a new power level token by transmitting an identity credential, time and location indicia when needed.

A system controls engine power by self-executing contracts with an authority. A distributed method is performed at a plurality of authority apparatus, power level lock change file servers, and engine control units. Each authority apparatus provides a policy object for each Engine Control Unit (ECU). An authority sets power levels for self-executing compliance with policy constraints. A power level lock change file (LockChangeFile) server checks against date time constraints and geo-location scope by its authorities. An ECU receives a power level token when time and location constraint(s) by at least one authority is within scope. A distributed method includes receiving space time constraints and determining a policy object and Authoritative LockChangeFile; receiving date, time, and location indicia from an ECU; determining the lowest power level consistent with the LockChangeFile; and requesting a new power level token by transmitting an identity credential, time and location indicia when needed.

A method and a device for monitoring a deviation of a first rotational speed of a first drive unit for an aircraft from a second rotational speed of an at least second drive unit of an aircraft. The monitoring of the deviation of the first rotational speed of the first drive unit from the second rotational speed of the at least second drive unit is carried out as a function of a comparison of a detection of a first event of the first drive unit to a detection of a second event of the at least second drive unit.

A method and a device for monitoring a deviation of a first rotational speed of a first drive unit for an aircraft from a second rotational speed of an at least second drive unit of an aircraft. The monitoring of the deviation of the first rotational speed of the first drive unit from the second rotational speed of the at least second drive unit is carried out as a function of a comparison of a detection of a first event of the first drive unit to a detection of a second event of the at least second drive unit.

A motor controller to control rotational speed of an output shaft of an electric motor. The motor controller includes a proportional controller and a time-optimal controller. The proportional controller controls the rotational speed when a present rotational position of the shaft is between a target rotational position and a switching point, inclusively. The time-optimal controller controls the rotational speed when the present rotational position is not between the target rotational position and the switching point. Also introduced herein are aspects pertaining to determining the switching point in a manner that minimizes overshooting the target rotational position while maximizing expediency at which the target rotational position is reached.

A motor controller to control rotational speed of an output shaft of an electric motor. The motor controller includes a proportional controller and a time-optimal controller. The proportional controller controls the rotational speed when a present rotational position of the shaft is between a target rotational position and a switching point, inclusively. The time-optimal controller controls the rotational speed when the present rotational position is not between the target rotational position and the switching point. Also introduced herein are aspects pertaining to determining the switching point in a manner that minimizes overshooting the target rotational position while maximizing expediency at which the target rotational position is reached.

A method and a device for monitoring a deviation of a first rotational speed of a first drive unit for an aircraft from a second rotational speed of an at least second drive unit of an aircraft. The monitoring of the deviation of the first rotational speed of the first drive unit from the second rotational speed of the at least second drive unit is carried out as a function of a comparison of a detection of a first event of the first drive unit to a detection of a second event of the at least second drive unit.

An ignition system for a tandem-type hybrid vehicle. The tandem-type hybrid vehicle comprises a plurality of engines (100, 110, 120, 130, 140, 150). The ignition system comprises: a plurality of ignition coils (101), each of the engines being configured to have at least one of the ignition coils, and each of the ignition coils comprising a primary winding and a secondary winding which are mutually matched; a single igniter (200) provided with a plurality of output ports (103) with the quantity corresponding to that of the plurality of ignition coils, each of the output ports being connected to the primary winding of one corresponding ignition coil so as to control the connection and disconnection of a current in the primary winding of the ignition coil; and an electronic control unit (300) for determining, according to a current power demand of the tandem-type hybrid vehicle, the engine to be started in the plurality of engines, determining the ignition coil to be boosted in the ignition coils in the engine to be started and issuing a corresponding ignition instruction, wherein the single igniter controls, according to the ignition instruction, the connection and disconnection of the current in the primary winding of the corresponding ignition coil to be boosted.

In order to address turbo lag at altitude, a vehicle boosts output torque of an internal combustion engine with electric motor torque generated from a battery. The residual charge of the battery is increased at altitude to provide a sufficient reserve for the corresponding increase in turbo lag. The invention is typically applied to a parallel hybrid vehicle.

In order to address turbo lag at altitude, a vehicle boosts output torque of an internal combustion engine with electric motor torque generated from a battery. The residual charge of the battery is increased at altitude to provide a sufficient reserve for the corresponding increase in turbo lag. The invention is typically applied to a parallel hybrid vehicle.