Abstract: Embodiments in include a system, a method, and a computer program product for performing intelligent load shedding for multi-channel processing system. The embodiments include a multi-channel processing system, wherein each channel of the multi-channel processing system includes a plurality of processors, and a plurality of links coupling each channel with each other channel in the multi-channel processing system, wherein the links are used to transmit status information of the plurality of processors. The embodiments also include a plurality of cooling elements coupled to each channel having the plurality of processors, wherein the plurality of cooling elements are configured to remove heat from the multi-channel processing system.

Abstract: An example actuator control system includes a variable differential transformer (VDT) configured to measure displacement of a motor, and a motor controller configured to control the motor based on displacement data from the VDT. A circuit card assembly (CCA) interconnects the VDT to the motor controller. The CCA includes memory storing configuration data of the VDT, and the CCA is configured to provide the configuration data to the motor controller to calibrate the motor controller for use of the VDT. A method of configuring a motor controller is also disclosed.

Abstract: A method for testing autonomous reconfiguration logic for an electromechanical actuator includes executing a plurality of test cases against a computer model configured and operable to implement autonomous reconfiguration logic for an electromechanical actuator including a plurality of electromechanical motors to generate a first set of test results. The method further includes executing the plurality of test cases against a programmable logic device configured and operable to implement the autonomous reconfiguration logic for the electromechanical actuator to generate a second set of test results and comparing the first set of test results to the second set of test results.

Abstract: A linear motor actuator includes a plurality of stators mounted stationary relative to one another along a common actuation axis. A translator rod is mounted to the stators for linear motion relative to the stators along the actuation axis, wherein each stator is magnetically coupled to the translator rod to drive motion of the translator rod along the actuation axis.

Abstract: An example actuator assembly includes an actuator configured to move a rod. A variable differential transformer (VDT) is situated adjacent to the actuator. The VDT includes a core coupled to the rod such that movement of the rod causes a corresponding movement of the core. A plurality of windings surround the core for measuring displacement of the core. A shield surrounds the plurality of windings and shields the plurality of windings from a magnetic field of the actuator. The shield having a maximum permeability of 50,000-500,000. A LVDT configuration method is also disclosed.

Abstract: A fly-by-wire system includes an electromechanical actuator which includes a plurality of electromechanical motors. Each of the plurality of electromechanical motors is configured and operable to exchange operating status information with the other redundant electromechanical motors within the actuator. Also, each one of the plurality of electromechanical actuators is configured and operable to automatically configure itself for optimal mode of operation based on the received operating status information of at least one of the other electromechanical motors. The fly-by-wire system further includes a flight control computer operatively connected to the plurality of electromechanical motors within the actuator.

Abstract: A method of detecting a fault in a sinusoidally controlled permanent magnet synchronous motor (PMSM). The method includes receiving a first rotor reference frame current demand, the first rotor reference frame current demand based on a current control for the PMSM and receiving a first rotor reference frame current feedback, the first rotor reference frame current feedback corresponding to the first rotor reference frame current demand received. The method also includes computing a first error of the rotor reference frame current based on the first rotor reference frame current demand and the first rotor reference frame current feedback and identifying a fault of the sinusoidally controlled PMSM if the first error exceeds a first selected threshold for a first selected duration.

Abstract: An example actuator control system includes an actuator, a plurality of motors configured to cooperatively operate the actuator, and a controller. The controller is configured to determine an output signal for controlling active ones of the motors during a current update cycle based on a first gain value, an integral contribution from the current update cycle, and an integral contribution from a preceding update cycle. The controller is configured to, based on a quantity of the motors that is active differing between the current and preceding update cycles, scale the integral contribution from the preceding update cycle for the output signal determination based on the first gain value and a second gain value from the preceding update cycle. A method of controlling a plurality of actuator motors is also disclosed.

Abstract: A method and control system that implements a particular aircraft harnessing for an aircraft is provided. The control system includes an effector Line-Replaceable Unit (LRU) including a first connection port, a second connection port, and a first interconnect wire internally connecting the first connection port and the second connection port, a first control LRU connected using a first harnessing to the effector LRU, and a second control LRU connected using a second harnessing to the effector LRU, wherein the first control LRU and the second control LRU are configured to communicate using the first interconnect wire in the effector LRU.

Abstract: A linear motor actuator includes a plurality of stators mounted stationary relative to one another along a common actuation axis. A translator rod is mounted to the stators for linear motion relative to the stators along the actuation axis, wherein each stator is magnetically coupled to the translator rod to drive motion of the translator rod along the actuation axis.

Abstract: One or more embodiments here relate to a processing platform for performing channel management and channel monitoring of a control channel. The processing platform includes a first microcontroller comprising a first core. The processing platform includes a second microcontroller comprising a second core. The second microcontroller is dissimilar to the first microcontroller. The first core is in an active state to perform the channel management of the control channel. The second core is in a monitor state to perform the channel monitoring of the control channel.

Abstract: A system for monitoring a motor includes a movable component having a plurality of permanent magnets. The system also includes a plurality of stators having phase windings and surrounding the movable component. The system also includes a plurality of current sensors each configured to detect a detected current flowing to a corresponding stator of the plurality of stators. The system also includes a monitor configured to receive the detected current, perform a comparison of the detected current from each of the plurality of stators, and to identify a loss of redundancy of the motor based on the comparison.

Abstract: One or more embodiments here relate to a processing platform for performing channel management and channel monitoring of a control channel. The processing platform includes a first microcontroller comprising a first core. The processing platform includes a second microcontroller comprising a second core. The second microcontroller is dissimilar to the first microcontroller. The first core is in an active state to perform the channel management of the control channel. The second core is in a monitor state to perform the channel monitoring of the control channel.

Abstract: A linear motor actuator includes a plurality of stators mounted stationary relative to one another along a common actuation axis. A translator rod is mounted to the stators for linear motion relative to the stators along the actuation axis, wherein each stator is magnetically coupled to the translator rod to drive motion of the translator rod along the actuation axis.

Abstract: A method and control system that implements a particular aircraft harnessing for an aircraft is provided. The control system includes an effector Line-Replaceable Unit (LRU) including a first connection port, a second connection port, and a first interconnect wire internally connecting the first connection port and the second connection port, a first control LRU connected using a first harnessing to the effector LRU, and a second control LRU connected using a second harnessing to the effector LRU, wherein the first control LRU and the second control LRU are configured to communicate using the first interconnect wire in the effector LRU.

Abstract: A power system includes a first power input, a second power input, a power output, a first ideal diode coupled to the a power input and a power output and a second ideal diode coupled to a second power input and the power output. The power system also includes a first switching circuit coupled to the first power input and the first ideal diode and a second switching circuit coupled to the second power input and the second ideal diode, the switching circuits operating as an open or a short circuit based on an input. The power system also includes a test controller coupled to the first switching circuit, the second switching circuit and the power output and configured to determine an operating status of the power system based on an input to the first switch, inputs to the second switch and the power output.

Abstract: A method for controlling a vehicle is provided. The method includes generating a digital control signal, generating a digital simulated signal based on the control signal, the digital simulated signal simulating one of a mechanical or analog input signal, converting the digital simulated signal into an analog signal, and controlling a control device of the vehicle using the analog signal.

Abstract: In one example, a method includes receiving, by a controller device from a master device operably connected to the controller device, a memory access request configured to request access to computer-readable memory of the controller device. The method further includes sampling, by the controller device, time-varying data received from a controlled device operably connected to the controller device, and generating, by the controller device in response to receiving the memory access request, an access key using the sampled time-varying data received from the controlled device. The method further includes transmitting, by the controller device, the generated access key to the master device, and enabling, by the controller device, access to the computer-readable memory of the controller device in response to data write commands received from the master device that include an access code based on the access key.

Abstract: A power system includes a first power input, a second power input, a power output, a first ideal diode coupled to the a power input and a power output and a second ideal diode coupled to a second power input and the power output. The power system also includes a first switching circuit coupled to the first power input and the first ideal diode and a second switching circuit coupled to the second power input and the second ideal diode, the switching circuits operating as an open or a short circuit based on an input. The power system also includes a test controller coupled to the first switching circuit, the second switching circuit and the power output and configured to determine an operating status of the power system based on an input to the first switch, inputs to the second switch and the power output.

Abstract: A linear actuator includes an actuator housing. The actuator housing includes a plurality of motors providing linear movement along a motor drive axis wherein the motor drive axes are parallel, and wherein the motors are within the housing. Each motor includes a stator for applying an electromagnetic force and a rod movable within the stator. The electromagnetic force from the stator drives the rod to extend from and retract into the stator along the motor drive axis of that motor.