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, 4907-4912More 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 ExpositionMore 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, 7878More 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) , 1769-1774More Information
Srichander R.;Walker B. (01-01-1993). Stochastic stability analysis for continuous-time fault tolerant control systems. International Journal of Control, 57 (2) , 433-452More 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) , 225-229More 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) , 1064-1074More Information
Wereley N.;Walker B. (01-01-1990). Approximate evaluation of semi-Markov chain reliability models. Reliability Engineering and System Safety, 28 (2) , 133-164More 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) , 820-831More 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) , 475-482More 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) , 207-212More 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) , 483-491More 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) , 62-70More 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) , 313-319More 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) , 696-697More 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) , 744-755More Information