Rockwell Collins Control Technologies, Inc.

Aurora Flight Sciences Corporation

Athena Technologies, Inc.

Rockwell Collins, Inc.

Other

David W Vos

Vladislav Gavrilets

Benjamin Russ

Michael D Piedmonte

Keith M Allen

Damien B Jourdan

Behnam Motazed

Ben T Ludington

Christopher M Boggs

Gregory E Mott

Allen D Wu

David E Clough

A system for controlling operation of an internal combustion engine includes a controller configured to send signals for controlling at least one of air-fuel ratio, spark-ignition timing, and fuel injection timing to an internal combustion engine. The system further includes a sensor configured to send a signal indicative of exhaust gas temperature to the controller. The system is configured to control at least one of the air-fuel ratio, spark-ignition timing, and fuel injection timing based on a signal indicative of at least one of an operating condition of the internal combustion engine and load on the internal combustion engine, and a difference between a target exhaust gas temperature and the signal indicative of the exhaust gas temperature.

System and method for control of internal combustion engine

A vehicle includes at least one propulsion member and a power generation system. The power generation system includes a power source and a transmission configured to provide torque to the at least one propulsion member. The power generation system further includes a control apparatus comprising an input device and a processor. The processor is configured to receive signals indicative of a power output command, a plurality of detected ambient air conditions, and a plurality of detected power generation system parameters. The processor is also configured to determine a plurality of power generation system control settings for improving efficiency of the vehicle based on at least one of signals indicative of the power output command, the signals indicative of the plurality of detected ambient air conditions, and the signals indicative of a plurality of power generation system parameters.

Apparatus and method for controlling power generation system

A system for determining the orientation of a fixture relative to the Earth includes at least one sensor configured to detect a celestial body and provide signals indicative of a plurality of positions of a detected celestial body relative to the sensor over a period of time. The system further includes a processor configured to receive information relating to a time and date associated with the period of time during which the celestial body is detected, and information relating to an expected relationship between the detected celestial body and the Earth at the time and date. The processor is further configured to determine the orientation of the fixture relative to the Earth based on signals from the at least one sensor, and the information relating to the time and date and the expected relationship between the detected celestial body and the Earth at the time and date.

System and method for determining orientation relative to earth

A system for creating a digital representation of a status of one or more air vehicles and of sensed external objects includes one or more air vehicles, one or more sensors coupled to each of the one or more air vehicles, and a processor. The processor is configured to determine navigation information associated with travel of each of the one or more air vehicles, and capture data associated with the sensed external objects sensed by the one or more sensors. The processor is further configured to identify and track the sensed external objects in the captured data, geo-locate the identified sensed external objects via dynamic landmarking, and dynamically update a landmark database. The processor is further configured to utilize the landmark database to control at least one or more functions in a respective air vehicle of the one or more air vehicles.

System and method for developing dynamic positional database for air vehicles and terrain features

A system for controlling power of a hybrid vehicle may include a controller configured to receive a signal indicative of a commanded acceleration for the hybrid vehicle and determine a potential for each of a power source, a generator, and an energy storage device to supply energy to achieve the commanded acceleration. The controller may be further configured to determine a cost associated with using each of the power source, the generator, and the energy storage device to achieve the commanded acceleration, and determine a combination of the power source, the generator, and the energy storage device that achieves the commanded acceleration at a lowest total cost. The controller may also be configured to provide a signal to at least one of the power source, the generator, and the energy storage device to achieve the commanded acceleration based on the determined combination.

System and method for controlling power in a hybrid vehicle using cost analysis

Apparatus for controlling the power output efficiency of a power generation system based on an operator input. A processor is coupled to the input means and (i) receives the generated operator command, (ii) receives a plurality of detected ambient air conditions, (iii) receives a plurality of detected engine. performance parameters, (iv) determines first and second engine control commands based on the received pilot thrust command, the detected ambient environmental conditions, and the engine performance parameters, and (v) outputs control commands to optimize the efficiency of the power generation system.

Optimization method for power generation systems

An image-augmented inertial navigation system includes an inertial navigation system configured to estimate a navigation state vector and an imager configured to output pixel signals associated with terrain features passing through a field view of the imager. The system further includes a processing unit configured to determine a distance from the imager to each of the pixel signals for a given image frame and to determine a distance between the imager and a centroid of one or more of the terrain features passing through the field of view of the imager for the given image frame. The processing unit is also configured to track each terrain feature as the terrain features pass through the field of view of the imager. The processing unit is further configured to update the navigation state vector of the inertial navigation system based on calculated NED coordinates position information of the tracked terrain features.

Image augmented inertial navigation system (IAINS) and method

A system for estimating at least one of position, attitude, and heading of a vehicle is disclosed. The system includes at least three gyroscopes configured to output a signal indicative of inertial angular rates around three mutually orthogonal axes of the vehicle and at least three accelerometers configured to output a signal indicative of accelerations along three mutually orthogonal axes of the vehicle. The system further includes a triaxial magnetometer configured to output a signal indicative of a projection of ambient magnetic field on three mutually orthogonal axes of the vehicle. The system also includes a sensor configured to output a signal indicative of vehicle altitude and a differential pressure sensor configured to output a signal indicative of airspeed of the vehicle. The system further includes a device configured to receive the signals and estimate at least of one of position, attitude, and heading of the vehicle.

Systems and methods for estimating position, attitude, and/or heading of a vehicle

A control system () for controlling velocity and attitude of a dynamic system () includes a velocity controller configured to receive a desired velocity command and output a velocity error in the form of Euler angle commands to an attitude controller system. The attitude controller system includes a converter () configured to receive the Euler angle commands and output a desired quaternion based on the Euler angle commands. The attitude controller system further includes an attitude error generator () configured to receive the desired quaternion and an estimated quaternion indicative of an estimated velocity and attitude of the dynamic system () and to output attitude errors associated with the dynamic system (). The attitude controller system also includes an attitude controller () configured to receive the attitude errors and to output error commands to the dynamic system () based on the attitude errors.

Systems and methods for controlling dynamic systems

Apparatus for controlling the power output efficiency of a power generation system based on an operator input. A processor is coupled to the input means and (i) receives the generated operator command, (ii) receives a plurality of detected ambient air conditions, (iii) receives a plurality of detected engine performance parameters, (iv) determines first and second engine control commands based on the received pilot thrust command, the detected ambient environmental conditions, and the engine performance parameters, and (v) outputs control commands to optimize the efficiency of the power generation system.

An image-augmented inertial navigation system (LAWS) mounted on a vehicle () includes an inertial navigation system (INS) configured to estimate a navigation state vector and an imager () configured to output pixel signals associated with terrain features passing through a field of view (x, y, z) of the imager. The system (IAINS) further includes a processing unit operatively connected to the inertial navigation system (INS) and the imager (). The processing unit is configured to sense a distance from the imager to a centroid of one or more of the terrain features passing though a field of view of the imager for a given image frame associated with the feature pixel signals. The processing unit is also configured to track each terrain feature as the terrain features pass through the field of view of the imager. The processing unit is further configured to update the navigation state vector of the inertial navigation system (INS) based on calculated NED (North, East, Down) coordinates position information of the inertial navigation system (INS) relative to the tracked terrain features.

Image-augmented inertial navigation system (IAINS) and method

A method and apparatus are provided for controlling a dynamic device having multi-inputs and operating in an environment having multiple operating parameters. A method of designing flight control laws using multi-input, multi-output feedback LTI'zation is also provided. The method includes steps of: (i) determining coordinates for flight vehicle equations of motion; (ii) transforming the coordinates for the flight vehicle equations of motion into a multi-input linear time invariant system; (iii) establishing control laws yielding the transformed equations of motion LTI; (iv) adjusting the control laws to obtain a desired closed loop behavior for the controlled system; and (v) converting the transformed coordinates control laws to physical coordinates.

Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation

A tool for removing retaining clips from a surface, and particularly from a horseshoe attached to an animal's hoof, that includes a first plier lever, a second plier lever, a pivot point at which the first and second plier levers are rotatably fastened, an upper jaw portion on the first plier lever where the upper jaw is a wedge, and a lower jaw portion on the second plier lever where the lower jaw has a face that contacts the wedge when the first and second plier levers are pivoted closed, thereby providing support for the surface from which the fastener is being removed. Also included are a method of removing retaining clips, particularly from a horseshoe attached to an animal's hoof.

Horse farrier tool

Method and apparatus for a fault tolerant automatic control system for a dynamic device having a sensor and a predetermined control algorithm include structure and steps for receiving a status signal from the sensor. Structure and steps are provided for transforming the sensor status signal and a predetermined reference signal into a linear time invariant coordinate system, generating a sensor estimate in the linear time invariant coordinate system based on the transformed sensor status signal and the transformed reference signal, transforming the sensor estimate into a physical coordinate system, detecting an error in the sensor status signal based on a comparison of the transformed sensor estimate and the sensor status signal, and reconfiguring the predetermined control algorithm based on the detected error. Preferably, the apparatus and method are implemented in an aircraft flight control system capable of detecting an aircraft sensor fault and reconfiguring the flight control program such that flight control surface actuators are commanded by ignoring or mitigating the failed sensor.

Growing community of inventors

Delaplane, VA, United States of America

David W Vos