Vehicle Or Aerospace Patents (Class 706/913)
-
Patent number: 11501033Abstract: A computer-implemented method for converting an architecture specification of a system to one or more functional performance requirements textual statements describing one or more functions of the system is provided. The computer-implemented method includes obtaining the architecture specification based on a predefined architecture model diagram type, wherein the architecture specification comprises a plurality of interconnected functional portions that describe the one or more functions of the system; mapping one or more of the plurality of interconnected functional portions to one or more portions of the one or more functional performance requirements textual statements based on a predefined format of a template functional performance requirements textual statement; and creating the one or more functional performance requirements textual statements based on the mapping.Type: GrantFiled: October 7, 2019Date of Patent: November 15, 2022Assignee: THE BOEING COMPANYInventors: William Scott Wardlaw, Michael E. Crow
-
Patent number: 10557433Abstract: A system for detecting a fault condition in a valvetrain of an engine is configured to measure one or more operating parameters associated with the engine and determine if the operating parameters satisfy pre-defined corresponding boundary conditions. If so, a pair of values of at least one performance parameter is measured corresponding to measurement on a first and second bank of cylinders present on the engine. The difference between the pair of values is determined and used to compute at least one measure of variation for the at least one performance parameter in a time segment. If the at least one measure of variation for the at least one performance parameter exceeds a pre-defined limit for the engine, the valvetrain is flagged as faulty.Type: GrantFiled: December 5, 2016Date of Patent: February 11, 2020Assignee: Caterpillar Inc.Inventors: Michael Campagna, Andrew Billing, Dereck Heffron, Brian Wheeler
-
Patent number: 8396730Abstract: To improve the scheduling and tasking of resources, the present disclosure describes an improved planning system and method for the allocation and management of resources. The planning system uses a branch and bound approach of tasking resources using a heuristic to expedite arrival at a deterministic solution. For each possible functional mode of the resources, an upper bound is determined. The upper bounds are employed in an objective function for the branch and bound process to determine the functional mode in which to place the resources and to determine movement paths for the resources, all in an environment where a hostile force may attempt to destroy the resources.Type: GrantFiled: March 23, 2011Date of Patent: March 12, 2013Assignee: Raytheon CompanyInventors: Deepak Khosla, Eric Huang, David L. Ii
-
Patent number: 8209083Abstract: A method for detecting faults in an aircraft is disclosed. The method involves predicting at least one state of the aircraft and tuning at least one threshold value to tightly upper bound the size of a mismatch between the at least one predicted state and a corresponding actual state of the non-faulted aircraft. If the mismatch between the at least one predicted state and the corresponding actual state is greater than or equal to the at least one threshold value, the method indicates that at least one fault has been detected.Type: GrantFiled: August 4, 2006Date of Patent: June 26, 2012Assignee: Honeywell International Inc.Inventors: Subhabrata Ganguli, George Papageorgiou, Sonja Glavaski-Radovanovic
-
Patent number: 8195345Abstract: The method for generating an integrated guidance law for aerodynamic missiles uses a strength Pareto evolutionary algorithm (SPEA)-based approach for generating an integrated fuzzy guidance law, which includes three separate fuzzy controllers. Each of these fuzzy controllers is activated in a unique region of missile interception. The distribution of membership functions and the associated rules are obtained by solving a nonlinear constrained multi-objective optimization problem in which final time, energy consumption, and miss distance are treated as competing objectives. A Tabu search is utilized to build a library of initial feasible solutions for the multi-objective optimization algorithm. Additionally, a hierarchical clustering technique is utilized to provide the decision maker with a representative and manageable Pareto-optimal set without destroying the characteristics of the trade-off front. A fuzzy-based system is employed to extract the best compromise solution over the trade-off curve.Type: GrantFiled: August 5, 2010Date of Patent: June 5, 2012Assignee: King Fahd University of Petroleum & MineralsInventors: Hanafy M. Omar, Mohammad A. Abido
-
Patent number: 8190307Abstract: The control optimization method for helicopters carrying suspended loads during hover flight utilizes a controller based on time-delayed feedback of the load swing angles. The controller outputs include additional displacements, which are added to the helicopter trajectory in the longitudinal and lateral directions. This simple implementation requires only a small modification to the software of the helicopter position controller. Moreover, the implementation of this controller does not need rates of the swing angles. The parameters of the controllers are optimized using the method of particle swarms by minimizing an index that is a function of the history of the load swing. Simulation results show the effectiveness of the controller in suppressing the swing of the slung load while stabilizing the helicopter.Type: GrantFiled: August 23, 2010Date of Patent: May 29, 2012Assignee: King Fahd University of Petroleum & MineralsInventor: Hanafy M. Omar
-
Patent number: 8185259Abstract: The fuzzy logic-based control method for helicopters carrying suspended loads utilizes a controller based on fuzzy logic membership distributions of sets of load swing angles. The anti-swing controller is fuzzy-based and has controller outputs that include additional displacements added to the helicopter trajectory in the longitudinal and lateral directions. This simple implementation requires only a small modification to the software of the helicopter position controller. The membership functions govern control parameters that are optimized using a particle swarm algorithm. The rules of the anti-swing controller are derived to mimic the performance of a time-delayed feedback controller. A tracking controller stabilizes the helicopter and tracks the trajectory generated by the anti-swing controller.Type: GrantFiled: August 23, 2010Date of Patent: May 22, 2012Assignee: King Fahd University of Petroleum & MineralsInventor: Hanafy M. Omar
-
Patent number: 7863961Abstract: An ECU serving as a transmission side and an ECU serving as a reception side are coupled to each other through communication lines and junction connectors. A diode in which a direction directed from a negative-side output terminal of the ECU serving as the transmission side to a positive-side output terminal thereof becomes a forward direction is provided between the positive-side output terminal and the negative-side output terminal.Type: GrantFiled: September 29, 2005Date of Patent: January 4, 2011Assignee: Yazaki CorporationInventor: Yasuhiro Tamai
-
Patent number: 7742854Abstract: A system for on-board anomaly resolution for a vehicle has a data repository. The data repository stores data related to different systems, subsystems, and components of the vehicle. The data stored is encoded in a tree-based structure. A query engine is coupled to the data repository. The query engine provides a user and automated interface and provides contextual query to the data repository. An inference engine is coupled to the query engine. The inference engine compares current anomaly data to contextual data stored in the data repository using inference rules. The inference engine generates a potential solution to the current anomaly by referencing the data stored in the data repository.Type: GrantFiled: October 17, 2006Date of Patent: June 22, 2010Assignee: Boeing Management CompanyInventors: Ronald M. Fussell, Julie J. Anderson
-
Patent number: 7698104Abstract: Articles and systems comprise a diagnostic symptom tree system for diagnosing a failing system element causing a symptom in a system-under-test. A diagnostic symptom tree comprises symptom roots and dependent lower function nodes and sub-function nodes. Element nodes depend from the function or sub-function nodes, and a plurality of penultimate failure mode leaves depend from the element nodes. The function and sub-function nodes and the failure mode leaves comprise test information. Responsive to positive test results, the diagnostic symptom tree is configured to identify a function or sub-function or element node associated to a lowest symptom tree node or failure mode leaf for which a test is positive, or advise that no failing function or sub-function or element is found. In one aspect of the invention, nodes may include parameter values allowing successive selections of the nodes of the symptom tree for test iterations according to the parameter values.Type: GrantFiled: June 23, 2008Date of Patent: April 13, 2010Assignee: International Business Machines CorporationInventors: Benoit Cousin, Jean-Lois Neyt
-
Patent number: 7584074Abstract: A method and system comprising a diagnostic symptom tree system for diagnosing a failing system element causing a symptom in a system-under-test. A diagnostic symptom tree comprises symptom roots and dependent lower function nodes and sub-function nodes. Element nodes depend from the function or sub-function nodes, and a plurality of penultimate failure mode leaves depend from the element nodes. The function and sub-function nodes and the failure mode leaves comprise test information. Responsive to positive test results, the diagnostic symptom tree is configured to identify a function or sub-function or element node associated to a lowest symptom tree node or failure mode leaf for which a test is positive, or advise that no failing function or sub-function or element is found. In one aspect of the invention, nodes may include parameter values allowing successive selections of the nodes of the symptom tree for test iterations according to the parameter values.Type: GrantFiled: June 19, 2007Date of Patent: September 1, 2009Assignee: International Business Machines CorporationInventors: Benoit Cousin, Jean-Lois Neyt
-
Patent number: 7449858Abstract: The present invention provides a diagnostics methodology and embedded electronic system that allows optimized low-frequency data sampling for EMA motoring subsystems in an operating vehicle. Each of the EMA motoring subsystems includes: an EMA; at least one motor for driving the EMA; and power controls for operating the motor, wherein the power controls includes a DSP controller for sampling and processing data at low-frequency sampling rates. The diagnostic methodology includes a method that has the steps of: determining an operational mode of the EMA motoring subsystem; selecting a sampling rate optimized for the determined operational mode; acquiring and processing data at the selected sampling rate; and analyzing the processed data to identify and classify a fault of the EMA motoring subsystem.Type: GrantFiled: June 5, 2006Date of Patent: November 11, 2008Assignee: The Boeing CompanyInventors: Jie Chang, Kirby Keller, Anhua Wang, Jiajia Zhang
-
Patent number: 7409317Abstract: A method and system comprising a diagnostic symptom tree system for diagnosing a failing system element causing a symptom in a system-under-test. A diagnostic symptom tree comprises symptom roots and dependent lower function nodes and sub-function nodes. Element nodes depend from the function or sub-function nodes, and a plurality of penultimate failure mode leaves depend from the element nodes. The function and sub-function nodes and the failure mode leaves comprise test information. Responsive to positive test results, the diagnostic symptom tree is configured to identify a function or sub-function or element node associated to a lowest symptom tree node or failure mode leaf for which a test is positive, or advise that no failing function or sub-function or element is found. In one aspect of the invention, nodes may include parameter values allowing successive selections of the nodes of the symptom tree for test iterations according to the parameter values.Type: GrantFiled: November 22, 2005Date of Patent: August 5, 2008Assignee: International Business Machines CorporationInventors: Benoit Cousin, Jean-Lois Neyt
-
Patent number: 7383236Abstract: A method to obtain the Pareto solutions that are specified by human preferences is suggested. The main idea is to convert the fuzzy preferences into interval-based weights. With the help of the dynamically-weighted aggregation method, it is shown to be successful to find the preferred solutions on two test functions with a convex Pareto front. Compared to the method described in “Use of Preferences for GA-based Multi-Objective Optimization” (Proceedings of 1999 Genetic and Evolutionary Computation Conference, pp. 1504-1510, 1999) by Cvetkovic et al., the method according to the invention is able to find a number of solutions instead of only one, given a set of fuzzy preferences over different objectives. This is consistent with the motivation of fuzzy logic.Type: GrantFiled: December 10, 2002Date of Patent: June 3, 2008Assignee: Honda Research Institute Europe GmbHInventors: Yaochu Jin, Bernhard Sendhoff
-
Patent number: 7369976Abstract: A design of a tire can be facilitated. An optimization apparatus 30 inputs known design parameters of the shape, structure, and pattern of a tire, and performances thereof by an experimental data input unit 40 and learns, as a conversion system of a neural network, a correlation between design parameters of the shape, structure, and pattern of the tire, and performances thereof. Ranges which constrain performances of the tire and design parameters of the shape, structure, and pattern of the tire, which are to be optimized, are inputted in an optimization item input unit 42, and the performances of the tire are predicted in an optimization calculation unit 34 from the design parameters of the shape, structure, and pattern of the tire by using the optimization item and models of the calculation unit 32, and an objective function is optimized until the objective function which is the performances of the tire is converged.Type: GrantFiled: August 8, 1997Date of Patent: May 6, 2008Assignee: Bridgestone CorporationInventor: Yukio Nakajima
-
Patent number: 7349889Abstract: A method and system for diagnosing a fault that includes a decision tree having a plurality of decision points wherein at least some of the plurality of decision points terminate in a resolution point representing a diagnosis for the fault. Also included is a plurality of queries each having at least a first response and a second response where each of the plurality of queries being associated with one of the plurality of decision points. The system also includes a knowledge base that includes a plurality of first images where each of the plurality of first images illustrate one of the first responses. A user interface is included for presenting the plurality of queries and the illustrative first images to a user. The user navigates the decision tree by responding to at least some of the plurality of queries by viewing the illustrative first images and basing a selection between the first response and the second response associated with said at least some of said queries on said illustrative first images.Type: GrantFiled: November 20, 2000Date of Patent: March 25, 2008Assignee: Rohm and Haas Electronic Materials LLCInventors: Eric R. Alling, Clare R. Sokolowski
-
Patent number: 7269504Abstract: System and method for guiding a driver of a vehicle (20) from a starting point to a destination point using an assignment of levels of urgency of navigation cues. The system comprises a navigation unit (38), a controller (22) and a user interface (42). The navigation unit (38) is capable of selecting a route between the starting point and the destination point. The navigation unit (38) is further capable of generating a plurality of navigation cues to guide the driver along the selected route. The controller (22) is connected to the navigation unit (38) and receives navigation cues. The controller (22) has an urgency calculator (40) that is capable of assigning a level of urgency to the navigation cues. The controller (22) may also have a workload manager (60) that is capable of classifying an activity state of the driver as well as updating the level of urgency of the navigation cue. The user interface (42) presents the navigation cues based on the level of urgency of the navigation cues.Type: GrantFiled: October 25, 2004Date of Patent: September 11, 2007Assignee: Motorola, Inc.Inventors: Judith Lee Gardner, Walton Fehr
-
Patent number: 7211982Abstract: The present invention provides a diagnostics methodology and embedded electronic system that allows optimized low-frequency data sampling for EMA motoring subsystems in an operating vehicle. Each of the EMA motoring subsystems includes: an EMA; at least one motor for driving the EMA; and power controls for operating the motor, wherein the power controls includes a DSP controller for sampling and processing data at low-frequency sampling rates. The diagnostic methodology includes a method that has the steps of: determining an operational mode of the EMA motoring subsystem; selecting a sampling rate optimized for the determined operational mode; acquiring and processing data at the selected sampling rate; and analyzing the processed data to identify and classify a fault of the EMA motoring subsystem.Type: GrantFiled: June 5, 2006Date of Patent: May 1, 2007Assignee: The Boeing CompanyInventors: Jie Chang, Kirby Keller, Anhua Wang, Jiajia Zhang
-
Patent number: 6947797Abstract: A system (830) and method (800) for diagnosing a malfunctioning machine. A fault event is selected (806) together with sequential operating parameter data (808) from a selectively focused time interval about the fault event for evaluation of a machine (810). The selectively focused time interval may include data occurring just before, just after, or spanning the fault event. Characterizing information such as slope, rate of change, and absolute sign of the data may be derived (809) from the operating parameter data over the selectively focused time interval and used in the diagnosis. The fault event and operating parameter data may be compared to existing cases in a case database (834). A set of rules (817) or candidate anomalies (841) may be executed over the operating parameter data to further improve the accuracy of the diagnosis.Type: GrantFiled: July 24, 2002Date of Patent: September 20, 2005Assignee: General Electric CompanyInventors: Jason Arthur Dean, Nicholas Edward Roddy
-
Patent number: 6799105Abstract: The present invention involves a system and method of controlling a variable steering ratio of a vehicle steer-by-wire system. The variable steering ratio control varies the steering ratio continuously according to steering angle and vehicle speed. The method comprises sensing an actual steering wheel angle and an actual speed of the vehicle and converting the actual steering wheel angle and vehicle speed into values in fuzzy sets based on a steering wheel angle and vehicle speed membership functions with linguistic term labels. The method further includes determining a corresponding degree of membership of the steering wheel angle and vehicle speed. The method further includes inferring a fuzzy road wheel reference angle output value by determining the degree of membership function for the road wheel reference angle using fuzzy rules based on the degrees of steering angle and the vehicle speed. The method further includes converting a fuzzy road wheel angle into an actual road wheel angle.Type: GrantFiled: October 1, 2002Date of Patent: September 28, 2004Assignee: Visteon Global Technologies, Inc.Inventors: Gregory J. Stout, Yixin Yao
-
Patent number: 6574613Abstract: A system and a method for diagnosis of engine conditions are proposed. In particular, the system and the method are directed to an extraction of features from different information sources and to their processing. These features, together with a series connection of two neural networks, form the crux of the system and method, so that a dependable diagnosis of engine conditions, particularly an error recognition is possible. As a result thereof, maintenance corresponding to the current engine condition is enabled.Type: GrantFiled: March 2, 2000Date of Patent: June 3, 2003Inventor: Jorge Moreno-Barragan
-
Patent number: 6556981Abstract: A method for detecting fires and reacting thereto. A stationary, earth orbit satellite, drone aircrafts or piloted aircraft contains infrared detectors and optical means for detecting fires. A computer in the satellite, drone or piloted aircraft and/or on the ground analyzes image signals of the areas being monitored and, upon detecting infrared radiation of varying intensity and shape, indicative that a fire has started, generates signals which are indicative of the coordinate locations of the fire, the extent of the fire, the shape of the area(s) burning, the direction of movement of the fires, the speed(s) of the flame fronts, smoke condition, intensity of the fire, fire ball location(s), etc. In one form, a camera generates image signals which are digitized and recorded. Expert system logic is used to prioritize dangerous areas to assist in directing fire fighting.Type: GrantFiled: July 23, 2001Date of Patent: April 29, 2003Inventors: Robert D. Pedersen, Jerome H. Lemelson
-
Patent number: 6405108Abstract: A process and system for developing an algorithm for predicting failures in a system, such as a locomotive, having a plurality of subsystems is provided. The process allows for conducting a failure mode analysis for a respective subsystem so as to identify target failure modes of the subsystem and/or collecting expert data relative to the respective subsystem. The process includes a step for identifying, based on the identified failure modes and/or the collected expert data, one or more signals to be monitored for measuring performance of the respective subsystem. A generating step allows for generating, based on the monitored signals, a predicting signal indicative of the presence of the identified target failure modes in the respective subsystem.Type: GrantFiled: October 28, 1999Date of Patent: June 11, 2002Assignee: General Electric CompanyInventors: Sagar Arvindbhai Patel, Vinay Bhaskar Jammu
-
Patent number: 6212470Abstract: A vehicle route guidance system considers driver preferences, vehicle parameters such as speed and performance capabilities in a navigation computer, and outputs flexible guidance instructions based on these considerations. The system monitors vehicle parameters such as current location and speed with sensors such as an odometer (109), a compass (115), and a GPS receiver (113). The system also determines the location of a vehicle maneuver and then, considering the former attributes with a model free mechanism, in this case a navigation computer with fuzzy inferencing (101), communicates to the driver instructing him how to manoeuver.Type: GrantFiled: June 7, 1994Date of Patent: April 3, 2001Assignee: Motorola, Inc.Inventors: Leslie G. Seymour, Michael Barnea, Allan Kirson
-
Patent number: 6023668Abstract: A process and system for determining the flight configurations of an aircraft are disclosed. The process includes the steps of defining various possible flight configurations of the aircraft, determining a plurality of flight phases representative of the flight configurations, determining a plurality of characteristic parameters capable of being measured on the aircraft, measuring values of the characteristic parameters for each of the flight phases of the aircraft, calculating a fuzziness index for each of the flight configurations from the measured values of the characteristic parameters for the flight phases, the fuzziness index being representative of the flight configuration in a specified metric system, and defining an actual flight phase of the aircraft.Type: GrantFiled: January 10, 1997Date of Patent: February 8, 2000Assignee: Eurocopter FranceInventor: Gerard Charles Louis Genoux