Abstract: A system and method that provides improved fault detection in turbine engines is disclosed. The fault detection system provides the ability to detect symptoms of engine faults based on a relatively limited number of engine parameters that are sampled relatively infrequently. The fault detection system includes a sensor data processor that receives engine sensor data during operation and augments the sensor data. The augmented data set is passed to a fuzzy logic inference system that determines the likelihood that a fault has occurred. The inference system output can then be passed to a diagnostic system where evaluation of the output may yield a detailed diagnostic result and a prediction horizon.

Abstract: A method for avoiding singularities in the movement of CMGs in an array of CMGs in a spacecraft includes a first step where a maneuver command to rotate a spacecraft orientation is received. Then, the torque needed to rotate the spacecraft's orientation is determined. Then, the torque is integrated to determine a momentum path. The momentum path is decomposed into a sequence of straight line segments. For each line segment, a unit vector along the straight line segments is determined. Then, it is determined if there is a continuous path connecting a start point and an end point of the line segment in a plane perpendicular to the unit vector. For each point along the path in the plane perpendicular to the unit vector, a set of gimbal angles is determined.

Abstract: A method for avoiding singularities in the movement of CMGs in an array of CMGs in a spacecraft includes a first step where a maneuver command to rotate a spacecraft orientation is received. Then, the torque needed to rotate the spacecraft's orientation is determined. Then, the torque is integrated to determine a momentum path. The momentum path is decomposed into a sequence of straight line segments. For each line segment, a unit vector along the straight line segments is determined. Then, it is determined if there is a continuous path connecting a start point and an end point of the line segment in a plane perpendicular to the unit vector. For each point along the path in the plane perpendicular to the unit vector, a set of gimbal angles is determined.

Abstract: A method and system for dynamically balancing a rotating system, such that sensor measurements and responses to control actions can be compiled utilizing one or more sensors associated with the rotating system. The rotating system may be represented utilizing sensor measurements and responses to control actions through an associated control model, such that the control model and the sensor measurements are determinative of future control actions. The rotating system may be perturbed utilizing a control action while improving a balance condition associated with the rotating system. Sensor data may be measured from one or more sensors associated with the rotating system. Responses thereof may be determined based on the control action. The sensor data may be manipulated in order to remove measurements and responses thereof that do not well-represent the rotating system.

Abstract: A method for dynamically balancing a rotating system through strategic control model updates, wherein said system contains sensors and sensor measurements whose responses to control actions are used to represent the system through a control model, where said control model and sensor measurements are used to determine future control actions is disclosed. The performance of the control model is evaluated using sensor measurements and responses; the evaluation is further used to determine if it is necessary to update the control model. The ongoing performance of the current control model is anticipated utilizing rate-of-change metrics obtained by evaluating said sensor measurements and responses. When a new control model is needed, further evaluation is done to determine if sensor measurements and responses are adequate for updating the control model.

Abstract: A method for dynamically balancing a rotating system through strategic control model updates, wherein said system contains sensors and sensor measurements whose responses to control actions are used to represent the system through a control model, where said control model and sensor measurements are used to determine future control actions is disclosed. The performance of the control model is evaluated using sensor measurements and responses; the evaluation is further used to determine if it is necessary to update the control model. The ongoing performance of the current control model is anticipated utilizing rate-of-change metrics obtained by evaluating said sensor measurements and responses. When a new control model is needed, further evaluation is done to determine if sensor measurements and responses are adequate for updating the control model.

Abstract: A method and system for dynamically balancing a rotating system or rotating device, such that sensor measurements and responses to control actions can be compiled utilizing one or more sensors associated with the rotating system is disclosed. The rotating system or rotating device may be represented utilizing sensor measurements and responses to control actions through an associated control model, such that the control model and the sensor measurements are determinative of future control actions. The rotating system may be perturbed utilizing a control action while improving a balance condition associated with the rotating system. Sensor data may be measured from one or more sensors associated with the rotating system. One or more responses thereof may be determined based on the control action. The sensor data may be manipulated in order to remove measurements and responses thereof that do not well represent the rotating system.

Abstract: A method for identifying resonance in a rotating system, wherein the rotating system includes sensors and sensor measurements thereof whose responses to control actions is utilized to represent the rotating system through a control model is disclosed. The control model determines actions required to balance the system (i.e., to drive sensor measurements to zero). The current state of the system is evaluated and recorded by obtaining current sensor readings from at least one sensor associated with the rotating device. The system model can then be used with at least one current sensor reading to calculate at least one predicted sensor reading due to changes in rotational speed of the rotating system. After changing the speed of the rotating system new sensor readings can be obtained and recorded.

Abstract: A method and system for balancing a rotating device or rotating system having a rotatable member and a shaft attached to the rotatable member, such that balancing is based on system response to simultaneous control actions to place mass, such as for example, fluid, at predetermined locations within the rotating system or rotating device. Mass can be simultaneously placed at predetermined locations within the rotating system. A system model of measured force and motion parameters can then be calculated in response to simultaneously placing mass at predetermined locations within the rotating system, in order to determine a required correction necessary to place the rotating system in a balanced state. Force can be measured at predetermined locations throughout the rotating system or rotating device in response to simultaneously placing the mass at the predetermined locations within the rotating system or rotating device.