Bruce Walker

Bruce K Walker

Research Support

Grant: #200-1Q-14U36188 Investigators:Walker, Bruce 02-08-2006 -01-31-2008 Department of the Air Force Jet Engines Diagnostics Role:PI $113,731.00 Closed Level:Federal

Grant: #PGS95836 Investigators:Walker, Bruce 07-01-2000 -06-30-2001 General Motors Corporation Passive Engine Gas Remission Valve Fault Diagnosis Using Model Based Parameter Estimation Role:PI $70,431.00 Closed Level:Industry

Grant: #TCS57774 Investigators:Walker, Bruce 04-01-1999 -12-31-1999 General Motors Corporation Passive Engine Gas Remission Valve Fault Diagnosis Using Model-Based Parameter Estimation Role:PI $59,358.00 Closed Level:Industry

Grant: #200-1O-14C43212 Investigators:Lee, Jay; Walker, Bruce 02-12-2008 -12-30-2008 General Electric Aviation Performance-Based Diagnostics, Prognostics, and Health Management for GE's Installed Fleet of Commercial Jet Engines: Phase I Role:PI $128,090.00 Closed Level:Industry

Grant: #200-18-14C43241 Investigators:Walker, Bruce 06-09-2008 -06-30-2009 Department of the Air Force Controls and Diagnostics Support Role:PI $42,472.00 Closed Level:Federal

Grant: #TECH-09-022 Investigators:Abdallah, Shaaban; Cohen, Kelly; Hamed, Awatef; Jeng, San-Mou; Jog, Milind; Khosla, Prem; Lee, Jay; Qian, Dong; Schulz, Mark; Shanov, Vesselin; Singh, Raj; Steckl, Andrew; Turner, Mark; Vasudevan, Vijay; Walker, Bruce 08-18-2008 -08-17-2013 Ohio Department of Development Intelligent Propulsion and Power Systems and Their Life Management Role:Collaborator $27,492,308.00 Active Level:State of Ohio

Publications

Peer Reviewed Publications

Gerlach A.;Kingston D.;Walker B. (01-01-2014. ) UAV navigation using predictive vector field control.Proceedings of the American Control Conference, , 4907-4912 More Information

Gerlach A.; Walker B. (09-16-2013. ) Directly controlling the sparsity of an interpolation matrix formed by compactly supported RBFNs .AIAA Infotech at Aerospace (I at A) Conference, ,

Gerlach A.; Walker B. (09-16-2013. ) Trajectory tracking by approximate inverse dynamics: An introduction to the IDRBF algorithm .AIAA Infotech at Aerospace (I at A) Conference, ,

Gerlach A.; Walker B. (09-16-2013. ) Trajectory tracking by approximate inverse dynamics: IDRBF computational considerations .AIAA Infotech at Aerospace (I at A) Conference, ,

Gerlach A.;Walker B. (12-01-2012. ) Accelerating robust 3D pose estimation using c*-images.50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, , More Information

Aull M.; Walker B. (12-01-2011. ) Development of a fuzzy system for jet engine diagnostics and comparison with a bayesian diagnostic s .AIAA Infotech at Aerospace Conference and Exhibit 2011, ,

Cohen K.; Lee J.; Walker B. (12-01-2011. ) Path planning of unmanned aerial vehicles in a dynamic environment .AIAA Infotech at Aerospace Conference and Exhibit 2011, ,

Gerlach A.;Walker B. (02-28-2011. ) Accelerating robust 3D pose estimation utilizing a graphics processing unit.Proceedings of SPIE - The International Society for Optical Engineering, , 7878 , More Information

Walker B.;Saraf A.;Godbole A. (12-01-2003. ) Robust flight control for coordinated turns .AIAA Guidance, Navigation, and Control Conference and Exhibit, ,

Moore K.T.;Naylor B.A.;Walker B.K.;Nayfeh A.;Khosla P.K. (01-01-1998. ) A simple model for and object-oriented simulation of interacting fluid and structural dynamics of fe .Computer Modeling and Simulation in Engineering, , 3 (2 ) ,111-122

Orkwis P.;Walker B.;Jeng S.;Khosla P.;Slater G.;Simitses G. (12-01-1997. ) Horizontal and vertical integration of design: An approach to curriculum revision .International Journal of Engineering Education, , 13 (3 ) ,220-226

Garcia-Velo J.;Walker B.K. (11-01-1997. ) Aerodynamic parameter estimation for high-performance aircraft using extended Kalman filtering .Journal of Guidance, Control, and Dynamics, , 20 (6 ) ,1257-1259

Walker B.;Wade J.;Orkwis P.;Jeng S.;Khosla P.;Slater G. (01-01-1997. ) Development of a proposed aerospace engineering curriculum for the twenty-first century .35th Aerospace Sciences Meeting and Exhibit, ,

Walker B.;Jeng S.;Orkwis P.;Slater G.;Khosla P.;Simitses G. (12-01-1995. ) Educating aerospace engineers for the twenty-first century: results of a survey .ASEE Annual Conference Proceedings, , 1 ,66-75

Orkwis P.;Jeng S.;Walker B.;Slater G.;Khosla P.;Simitses G. (12-01-1995. ) Designing a new aerospace engineering curriculum: the process .ASEE Annual Conference Proceedings, , 1 ,76-83

García-Velo J.;Walker B. (01-01-1995. ) Aerodynamic parameter estimation for high-performance aircraft using extended Kalman filtering .20th Atmospheric Flight Mechanics Conference, , 593-600

Walker B.;Huang K. (01-01-1995. ) FDI by extended Kalman filter parameter estimation for an industrial actuator benchmark.Control Engineering Practice, , 3 (12 ) ,1769-1774 More Information

Srichander R.;Walker B. (01-01-1993. ) Stochastic stability analysis for continuous-time fault tolerant control systems.International Journal of Control, , 57 (2 ) ,433-452 More Information

Walker B.K.;Baumgartner E.T. (12-01-1992. ) Parameter estimation by nonlinear smoothing for fault monitoring on rocket engines .IFAC Symposia Series, , (6 ) ,191-198

Srichander R.;Walker B.K. (12-01-1992. ) Selecting thresholds for sequential fault detection tests .IFAC Symposia Series, , (6 ) ,165-172

Hill B.;Walker B. (12-01-1991. ) Approximate effect of parameter pseudonoise intensity on rate of convergence for EKF parameter estim .Proceedings of the IEEE Conference on Decision and Control, , 2 ,1690-1697

Srichander R.;Walker B.K. (12-01-1991. ) Stochastic stability analysis for continuous time fault tolerant control systems .Proceedings of the American Control Conference, , 1 ,493-501

Vaughan R.;Bergmann E.;Walker B. (01-01-1991. ) Collision detection for spacecraft proximity operations.Journal of Guidance, Control, and Dynamics, , 14 (2 ) ,225-229 More Information

Baumgartner E.T.;Walker B.K. (01-01-1990. ) Nonlinear smoothing for the continuous-discrete problem with application to rocket health monitoring .Guidance, Navigation and Control Conference, 1990, , 797-807

Hall S.;Walker B. (01-01-1990. ) Orthogonal series generalized likelihood ratio test for failure detection and isolation.Journal of Guidance, Control, and Dynamics, , 13 (6 ) ,1064-1074 More Information

Wereley N.;Walker B. (01-01-1990. ) Approximate evaluation of semi-Markov chain reliability models.Reliability Engineering and System Safety, , 28 (2 ) ,133-164 More Information

Srichander R.;Walker B.K. (12-01-1989. ) Approximate algorithm for evaluation of semi-Markov reliability models .2653-2659

Villalba M.;Walker B. (01-01-1989. ) Spectrum Manipulation for Improved Resolution.IEEE Transactions on Acoustics, Speech, and Signal Processing, , 37 (6 ) ,820-831 More Information

Walker B.;Wereley N.;Luppold R.;Gai E. (01-01-1989. ) Effects of Redundancy Management on Reliability Modeling.IEEE Transactions on Reliability, , 38 (4 ) ,475-482 More Information

Wereley N.;Walker B. (12-01-1988. ) Approximate semi-Markov chain reliability models .Proceedings of the IEEE Conference on Decision and Control, , 2322-2329

Richfield R.;Walker B.;Bergmann E. (01-01-1988. ) Input selection for a second-order mass property estimator.Journal of Guidance, Control, and Dynamics, , 11 (3 ) ,207-212 More Information

Bergmann E.;Walker B.;Levy D. (01-01-1987. ) Mass property estimation for control of asymmetrical satellites.Journal of Guidance, Control, and Dynamics, , 10 (5 ) ,483-491 More Information

Mangoubi R.;Gai E.;Walker B. (12-01-1986. ) ON THE PERFORMANCE ANALYSIS OF A REAL-TIME DISTRIBUTED COMPUTER SYSTEM. 529-535

Richfield R.;Walker B.;Bergmann E. (12-01-1986. ) INPUT SELECTION AND CONVERGENCE TESTING FOR A SECOND ORDER MASS PROPERTY ESTIMATOR. AIAA Paper, , 57-67

Walker B.;Coetsee J. (12-01-1985. ) STABILITY OF ADAPTIVE CONTROL ALGORITHMS - THEORETICAL EXAMINATION AND SIMULATION FOR F-4 FLIGHT CON .AIAA Paper, , 821-827

Walker B.;Gerber D. (12-01-1985. ) EVALUATION OF FAULT-TOLERANT PERFORMANCE BY APPROXIMATE TECHNIQUES. IFAC Proceedings Series, , (7 ) ,1937-1942

Bergmann E.;Walker B.;Levy D. (12-01-1985. ) MASS PROPERTY ESTIMATION FOR CONTROL OF ASYMMETRICAL SATELLITES. AIAA Paper, , 83-93

Bergmann E.V.;Walker B.K.;Levy D.R. (01-01-1985. ) Mass property estimation for control of asymmetrical satellites .Guidance, Navigation and Control Conference, 1985, ,

Walker B.;Gai E.;Desai M. (01-01-1985. ) A fault-tolerant approach to helicopter swashplate control.Journal of Guidance, Control, and Dynamics, , 8 (1 ) ,62-70 More Information

Luppold R.;Gai E.;Walker B. (12-01-1984. ) EFFECTS OF REDUNDANCY MANAGEMENT ON RELIABILITY MODELLING. Proceedings of the American Control Conference, , 3 ,1763-1770

Schabowsky R.;Gai E.;Walker B.;Lala J.;Motyka P. (12-01-1984. ) EVALUATION METHODOLOGIES FOR AN ADVANCED INFORMATION PROCESSING SYSTEM. AIAA Paper, , 217-224

Desai M.; Fogel E.; Nevins J.; Walker B.; Whitney D. (01-01-1984. ) ADAPTIVE CONTROL, LEARNING, AND COST EFFECTIVE SENSOR SYSTEMS FOR ROBOTIC OR ADVANCED AUTOMATION SYS .983-994

Desai M.; Fogel E.; Nevins J.; Walker B.; Whitney D. (12-01-1983. ) ADAPTIVE CONTROL, LEARNING AND COST EFFECTIVE SENSOR SYSTEMS FOR ROBOTIC OR ADVANCED AUTOMATION SYST .335-350

Walker B.;Gai E. (01-01-1979. ) Fault detection threshold determination technique using markov theory.Journal of Guidance, Control, and Dynamics, , 2 (4 ) ,313-319 More Information

Gai E.;Adams M.;Walker B.;Smestad T. (01-01-1978. ) Correction to “Determination of Failure Thresholds in Hybrid Navigation”.IEEE Transactions on Aerospace and Electronic Systems, , AES-14 (4 ) ,696-697 More Information

Gai E.;Adams M.;Walker B. (01-01-1976. ) Determination of Failure Thresholds in Hybrid Navigation.IEEE Transactions on Aerospace and Electronic Systems, , AES-12 (6 ) ,744-755 More Information