Patents by Inventor Anthony J. Calise
Anthony J. Calise has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 9494941Abstract: A method of guiding aerial vehicles to a target site in adverse weather conditions wherein the method regulates the range indirectly by regulating heading error to an offset target that revolves around the true target site. The improved guidance architecture is effective in adverse weather conditions, such as high winds.Type: GrantFiled: June 28, 2010Date of Patent: November 15, 2016Assignee: Luminati Aerospace LLCInventor: Anthony J. Calise
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Patent number: 9058028Abstract: Systems and methods for adaptive control are disclosed. The systems and methods can control uncertain dynamic systems. The control system can comprise a controller that employs a parameter dependent Riccati equation. The controller can produce a response that causes the state of the system to remain bounded. The control system can control both minimum phase and non-minimum phase systems. The control system can augment an existing, non-adaptive control design without modifying the gains employed in that design. The control system can also avoid the use of high gains in both the observer design and the adaptive control law.Type: GrantFiled: April 30, 2012Date of Patent: June 16, 2015Assignee: Georgia Tech Research CorporationInventors: Kilsoo Kim, Tansel Yucelen, Anthony J. Calise
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Patent number: 8996195Abstract: An adaptive control system is disclosed. The control system can control uncertain dynamic systems. The control system can employ one or more derivative-free adaptive control architectures. The control system can further employ one or more derivative-free weight update laws. The derivative-free weight update laws can comprise a time-varying estimate of an ideal vector of weights. The control system of the present invention can therefore quickly stabilize systems that undergo sudden changes in dynamics, caused by, for example, sudden changes in weight. Embodiments of the present invention can also provide a less complex control system than existing adaptive control systems. The control system can control aircraft and other dynamic systems, such as, for example, those with non-minimum phase dynamics.Type: GrantFiled: April 12, 2012Date of Patent: March 31, 2015Assignee: Georgia Tech Research CorporationInventors: Tansel Yucelen, Kilsoo Kim, Anthony J. Calise
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Patent number: 8660717Abstract: A method of approximately correcting a vehicle's guidance system command for the disturbing effects of the medium through which it is moving, without having to sense or estimate the speed and direction of that medium. The correction is determined by taking the ratio of two scalar quantities: the speed of the vehicle relative to the medium, which can be estimated from the known fluid dynamic characteristics of the vehicle, divided by an approximation of inertial speed, which can be obtained using one or more on-board sensors such as a GPS, thus increasing transient performance of the vehicle moving through the fluid medium.Type: GrantFiled: March 10, 2010Date of Patent: February 25, 2014Assignee: Atair AerospaceInventor: Anthony J. Calise
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Publication number: 20120265367Abstract: An adaptive control system is disclosed. The control system can control uncertain dynamic systems. The control system can employ one or more derivative-free adaptive control architectures. The control system can further employ one or more derivative-free weight update laws. The derivative-free weight update laws can comprise a time-varying estimate of an ideal vector of weights. The control system of the present invention can therefore quickly stabilize systems that undergo sudden changes in dynamics, caused by, for example, sudden changes in weight. Embodiments of the present invention can also provide a less complex control system than existing adaptive control systems. The control system can control aircraft and other dynamic systems, such as, for example, those with non-minimum phase dynamics.Type: ApplicationFiled: April 12, 2012Publication date: October 18, 2012Applicant: Georgia Tech Research CorporationInventors: Tansel Yucelen, Kilsoo Kim, Anthony J. Calise
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Publication number: 20110029163Abstract: A method of approximately correcting a vehicle's guidance system command for the disturbing effects of the medium through which it is moving, without having to sense or estimate the speed and direction of that medium. The correction is determined by taking the ratio of two scalar quantities: the speed of the vehicle relative to the medium, which can be estimated from the known fluid dynamic characteristics of the vehicle, divided by an approximation of inertial speed, which can be obtained using one or more on-board sensors such as a GPS, thus increasing transient performance of the vehicle moving through the fluid medium.Type: ApplicationFiled: March 10, 2010Publication date: February 3, 2011Applicant: ATAIR AEROSPACEInventor: Anthony J. Calise
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Publication number: 20100332066Abstract: A method of guiding aerial vehicles to a target site in adverse weather conditions wherein the method regulates the range indirectly by regulating heading error to an offset target that revolves around the true target site. The improved guidance architecture is effective in adverse weather conditions, such as high winds.Type: ApplicationFiled: June 28, 2010Publication date: December 30, 2010Applicant: Atair AerospaceInventor: Anthony J. Calise
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Patent number: 7853338Abstract: The invention comprises apparatuses and methods for providing the capability to stabilize and control a non-minimum phase, nonlinear plant with unmodeled dynamics and/or parametric uncertainty through the use of adaptive output feedback. A disclosed apparatus can comprise a reference model unit for generating a reference model output signal ym The apparatus can comprise a combining unit that combines and differences a plant output signal y of a non-minimum phase plant for which not all of the states can be sensed, and a plant output signal y, to generate an output error signal {tilde over (y)}. The apparatus can further comprise an adaptive control unit for generating an adaptive control signal uad used to control the plant.Type: GrantFiled: August 27, 2007Date of Patent: December 14, 2010Assignee: Georgia Tech Research CorporationInventors: Naira Hovakimyan, Anthony J Calise, Bong-Jun Yang
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Patent number: 7769703Abstract: A system in accordance with the invention uses an adaptive element to augment a filter for tracking an observed system. The adaptive element only requires a single neural network and does not require an error observer. The adaptive element provides robustness to parameter uncertainty and unmodeled dynamics present in the observed system for improved tracking performance over the filter alone. The adaptive element can be implemented with a linearly parameterized neural network, whose weights are adapted online using error residuals generated from the Filter. Boundedness of the signals generated by the system can be proven using Lyapunov's direct method and a backstepping argument. A related apparatus and method are also disclosed.Type: GrantFiled: November 18, 2006Date of Patent: August 3, 2010Assignee: Georgia Tech Research CorporationInventors: Anthony J. Calise, Venkatesh K. Madyastha
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Publication number: 20100030716Abstract: A system in accordance with the invention uses an adaptive element to augment a filter for tracking an observed system. The adaptive element only requires a single neural network and does not require an error observer. The adaptive element provides robustness to parameter uncertainty and unmodeled dynamics present in the observed system for improved tracking performance over the filter alone. The adaptive element can be implemented with a linearly parameterized neural network, whose weights are adapted online using error residuals generated from the Filter. Boundedness of the signals generated by the system can be proven using Lyapunov's direct method and a backstepping argument. A related apparatus and method are also disclosed.Type: ApplicationFiled: November 18, 2006Publication date: February 4, 2010Applicant: Georgia Tech Research CorporationInventors: Anthony J. Calise, Venkatesh K. Madyastha
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Publication number: 20090128408Abstract: A method of computing an antenna pointing direction for an inertial navigation unit (INU) utilizing a global positioning system (GPS) signal during periods of GPS signal outage includes determining antenna pointing error of magnitude and phase information. The phase information is obtained by detecting the angle where a signal to noise ratio of the antenna passes through a minimum level, and wherein the magnitude information is obtained by calculating the difference between the maximum and minimum signal to noise ratio of the antenna measured over one conical cycle of rotation of the antenna about an axis that is not parallel to a vector pointing from an antenna center to a GPS signal transmitting satellite. During periods of GPS signal outage, the determined magnitude and phase information is used to cause a nominal antenna beam axis to move by an amount that depends on the determined magnitude information in a direction defined by the determined phase information.Type: ApplicationFiled: July 17, 2008Publication date: May 21, 2009Applicant: ATAIR AEROSPACEInventors: Daniel J. Preston, Anthony J. Calise
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Patent number: 7418432Abstract: An adaptive control system (ACS) uses direct output feedback to control a plant. The ACS uses direct adaptive output feedback control developed for highly uncertain nonlinear systems, that does not rely on state estimation. The approach is also applicable to systems of unknown, but bounded dimension, whose output has known, but otherwise arbitrary relative degree. This includes systems with both parameter uncertainty and unmodeled dynamics. The result is achieved by extending the universal function approximation property of linearly parameterized neural networks to model unknown system dynamics from input/output data. The network weight adaptation rule is derived from Lyapunov stability analysis, and guarantees that the adapted weight errors and the tracking error are bounded.Type: GrantFiled: April 12, 2005Date of Patent: August 26, 2008Assignee: Georgia Tech Research CorporationInventors: Anthony J. Calise, Naira Hovakimyan, Moshe Idan
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Patent number: 7415311Abstract: A computer system for controlling a nonlinear physical process. The computer system comprises a linear controller and a neural network. The linear controller receives a command signal for control of the nonlinear physical process and a measured output signal from the output of the nonlinear physical process. The linear controller generates a control signal based on the command signal, a measured output signal, and a fixed linear model for the process. The neural network receives the control signal from the linear controller and the measured output signal from the output of the nonlinear physical process. The neural network uses the measured output signal to modify the connection weights of the neural network. The neural network also generates a modified control signal supplied to the linear controller to iterate a fixed point solution for the modified control signal used to control the nonlinear physical process.Type: GrantFiled: January 4, 2007Date of Patent: August 19, 2008Assignee: Guided Systems Technologies, Inc.Inventors: Anthony J. Calise, Byoung-Soo Kim, J. Eric Corban
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Patent number: 7218973Abstract: The invention includes an adaptive control system used to control a plant. The adaptive control system includes a hedge unit that receives at least one control signal and a plant state signal. The hedge unit generates a hedge signal based on the control signal, the plant state signal, and a hedge model including a first model having one or more characteristics to which the adaptive control system is not to adapt, and a second model not having the characteristic(s) to which the adaptive control system is not to adapt. The hedge signal is used in the adaptive control system to remove the effect of the characteristic from a signal supplied to an adaptation law unit of the adaptive control system so that the adaptive control system does not adapt to the characteristic in controlling the plant.Type: GrantFiled: June 23, 2003Date of Patent: May 15, 2007Assignee: Georgia Tech Research CorporationInventors: Eric Norman Johnson, Anthony J. Calise
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Patent number: 7177710Abstract: A computer system for controlling a nonlinear physical process. The computer system comprises a linear controller and a neural network. The linear controller receives a command signal for control of the nonlinear physical process and a measured output signal from the output of the nonlinear physical process. The linear controller generates a control signal based on the command signal, a measured output signal, and a fixed linear model for the process. The neural network receives the control signal from the linear controller and the measured output signal from the output of the nonlinear physical process. The neural network uses the measured output signal to modify the connection weights of the neural network. The neural network also generates a modified control signal supplied to the linear controller to iterate a fixed point solution for the modified control signal used to control the nonlinear physical process.Type: GrantFiled: June 7, 2005Date of Patent: February 13, 2007Assignee: Guided Systems Technologies, Inc.Inventors: Anthony J. Calise, Byoung-Soo Kim
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Patent number: 6904422Abstract: An adaptive control system (ACS) uses direct output feedback to control a plant. The ACS uses direct adaptive output feedback control developed for highly uncertain nonlinear systems, that does not rely on state estimation. The approach is also applicable to systems of unknown, but bounded dimension, whose output has known, but otherwise arbitrary relative degree. This includes systems with both parameter uncertainty and unmodeled dynamics. The result is achieved by extending the universal function approximation property of linearly parameterized neural networks to model unknown system dynamics from input/output data. The network weight adaptation rule is derived from Lyapunov stability analysis, and guarantees that the adapted weight errors and the tracking error are bounded.Type: GrantFiled: May 25, 2001Date of Patent: June 7, 2005Assignee: Georgia Tech Research CorporationInventors: Anthony J. Calise, Naira Hovakimyan, Moshe Idan
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Patent number: 6757570Abstract: A process and neural network architecture for on-line adjustment of the weights of the neural network in a manner that corrects errors made by a nonlinear controller designed based on a model for the dynamics of a process under control. A computer system is provided for controlling the dynamic output response signal of a nonlinear physical process, where the physical process is represented by a fixed model of the process. The computer system includes a controlled device for responding to the output response signal of the system. The computer system also includes a linear controller for providing a pseudo control signal that is based on the fixed model for the process and provides a second controller, connected to the linear controller, for receiving the pseudo control signal and for providing a modified pseudo control signal to correct for the errors made in modeling the nonlinearities in the process. A response network is also included as part of the computer system.Type: GrantFiled: May 31, 2000Date of Patent: June 29, 2004Assignee: Guided Systems Technologies, Inc.Inventors: Anthony J. Calise, Byoung-Soo Kim, J. Eric Corban
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Publication number: 20040088059Abstract: The invention includes an adaptive control system used to control a plant. The adaptive control system includes a hedge unit that receives at least one control signal and a plant state signal. The hedge unit generates a hedge signal based on the control signal, the plant state signal, and a hedge model including a first model having one or more characteristics to which the adaptive control system is not to adapt, and a second model not having the characteristic(s) to which the adaptive control system is not to adapt. The hedge signal is used in the adaptive control system to remove the effect of the characteristic from a signal supplied to an adaptation law unit of the adaptive control system so that the adaptive control system does not adapt to the characteristic in controlling the plant.Type: ApplicationFiled: June 23, 2003Publication date: May 6, 2004Applicant: Georgia Tech Reseach CorporationInventors: Eric Norman Johnson, Anthony J. Calise
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Patent number: 6618631Abstract: The invention includes an adaptive control system used to control a plant. The adaptive control system includes a hedge unit that receives at least one control signal and a plant state signal. The hedge unit generates a hedge signal based on the control signal, the plant state signal, and a hedge model including a first model having one or more characteristics to which the adaptive control system is not to adapt, and a second model not having the characteristic(s) to which the adaptive control system is not to adapt. The hedge signal is used in the adaptive control system to remove the effect of the characteristic from a signal supplied to an adaptation law unit of the adaptive control system so that the adaptive control system does not adapt to the characteristic in controlling the plant.Type: GrantFiled: May 31, 2000Date of Patent: September 9, 2003Assignee: Georgia Tech Research CorporationInventors: Eric Norman Johnson, Anthony J. Calise
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Patent number: 6611823Abstract: Methods and systems for backlash compensation. Restrictive assumptions on the backlash nonlinearity (e.g. the same slopes of the lines, etc.) are not required. The compensator scheme has dynamic inversion structure, with a neural network in the feedforward path that approximates the backlash inversion error plus filter dynamics needed for backstepping design. The neural network controller does not require preliminary off-line training. Neural network tuning is based on a modified Hebbian tuning law, which requires less computation than backpropagation. The backstepping controller uses a practical filtered derivative, unlike the usual differentiation required by earlier backstepping routines. Rigorous stability proofs are given using Lyapunov theory. Simulation results show that the proposed compensation scheme is an efficient way of improving the tracking performance of a vast array of nonlinear systems with backlash.Type: GrantFiled: April 20, 2000Date of Patent: August 26, 2003Assignee: Board of Regents, The University of Texas SystemInventors: Rastko R. Selmic, Frank L. Lewis, Anthony J. Calise, Michael B. McFarland