Research Support
Grant: #OSGC Investigators:Slater, Gary 09-01-1994 -08-31-2007 National Aeronautics and Space Administration Ohio Space Grant Consortium Scholarships and Fellowships Role:PI $416,381.00 Closed Level:Federal
Grant: #NCC5-728 Investigators:Slater, Gary; Williams, Trevor 07-01-2003 -06-30-2007 National Aeronautics and Space Administration Collision Avoidance and Safe Mode for Satellite Formations Role:Collaborator $179,518.00 Closed Level:Federal
Grant: #NNA06CB04G Investigators:Slater, Gary 04-01-2006 -04-30-2007 National Aeronautics and Space Administration Approaches to Multi-center Based Air Traffic Management Role:PI $102,678.00 Closed Level:Federal
Grant: #NAG -2-1581/ltr Investigators:Slater, Gary 09-15-2002 -12-31-2005 National Aeronautics and Space Administration Aircraft and Airspace Modeling: Approaches to Capacity Enhancement in Air Traffic Management Role:PI $171,520.00 Closed Level:Federal
Grant: #NCE Investigators:Slater, Gary 09-01-1999 -07-31-2002 National Aeronautics and Space Administration Advanced Trajectory Analysis with Application to Air Traffic Control Role:PI $142,203.00 Closed Level:Federal
Grant: #PO 200-1Q-14H45632 Investigators:Slater, Gary 10-01-2000 -12-30-2000 General Electric Company Undercowl Temperature Impact Investigation Role:PI $21,244.00 Closed Level:Industry
Grant: #NGT2-52205 Suppl #2 Investigators:Slater, Gary 09-01-1995 -08-31-1999 National Aeronautics and Space Administration Control Strategies for the Departure Problem in Air Traffic Management Role:PI $66,000.00 Closed Level:Federal
Grant: #NCE Investigators:Slater, Gary 07-01-1998 -12-15-2000 General Electric Company Simulation of Electromechanical Position Sensors Role:PI $25,000.00 Closed Level:Industry
Grant: #FY 2007-08 Investigators:Schaffner, Grant; Slater, Gary 09-01-2007 -08-31-2013 National Aeronautics and Space Administration Ohio Space Grant Role:PI $319,150.00 Active Level:Federal
Grant: #4103-21918 Investigators:Slater, Gary 01-01-2008 -12-31-2010 National Aeronautics and Space Administration Transition to Superdensity Operations- 2015 Timeframe Role:PI $122,549.00 Closed Level:Federal
Grant: #Ohio Innovation Partnership Investigators:Gaffney, James; Slater, Gary 07-01-2012 -06-30-2014 Ohio Board of Regents Choose Ohio First Scholarship Program 11.16 Role:Collaborator $86,100.00 Active Level:State of Ohio
Publications
Peer Reviewed Publications
Slater G.L. (12-01-2009). Using the parallel offset function to achieve required delay. 9th AIAA Aviation Technology, Integration and Operations (ATIO) Conference, Aircraft Noise and Emissions Reduction Symposium (ANERS)
Slater G.L. (12-01-2009). Study on variations in vertical profile for CDA descents. 9th AIAA Aviation Technology, Integration and Operations (ATIO) Conference, Aircraft Noise and Emissions Reduction Symposium (ANERS)
Saraf A.P.;Slater G.L. (09-01-2008). Adaptive Eulerian modeling for air traffic flow management. Journal of Aircraft, 45 (5) , 1585-1600More Information
Saraf A.P.;Slater G.L. (01-01-2008). Optimal dynamic scheduling of aircraft arrivals at congested airports. Journal of Guidance, Control, and Dynamics, 31 (1) , 53-65More Information
Saraf A.P.;Slater G.L. (12-24-2007). Adaptive Eulerian model for optimal air traffic flow management. Collection of Technical Papers - 7th AIAA Aviation Technology, Integration, and Operations Conference, 2, 1632-1653
Saraf A.P.;Slater G.L. (12-01-2007). Adaptive eulerian model for optimal air traffic flow management. Collection of Technical Papers - 7th AIAA Aviation Technology, Integration, and Operations Conference, 1
Saraf A.P.;Slater G.L. (12-01-2006). An efficient combinatorial optimization algorithm for optimal scheduling of aircraft arrivals at con. IEEE Aerospace Conference Proceedings, 2006
Saraf A.P.;Slater G.L. (12-01-2006). Combined eulerian-lagrangian two-level control system for optimal air traffic flow management. Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006, 3, 1711-1723
Slater G.L.;Byram S.M.;Williams T.W. (09-01-2006). Collision avoidance for satellites in formation flight. Journal of Guidance, Control, and Dynamics, 29 (5) , 1140-1146More Information
Alonso E.;Slater G.L. (12-01-2005). Control design and implementation for the self-separation of in-trail aircraft. Collection of Technical Papers - AIAA 5th ATIO and the AIAA 16th Lighter-than-Air Systems Technology Conference and Balloon Systems Conference, 2, 972-979
Williams T.;Slater G. (01-01-2005). Steady-state matched model reduction for flexible structures with accelerometer measurements. Journal of Guidance, Control, and Dynamics, 28 (2) , 360-363More Information
Slater G.L.;Yang D. (12-01-2004). Dynamic optimization of delay distribution in an uncertain environment. Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference, 4, 2231-2243
Slater G.L.;Byram S.M.;Williams T.W. (12-01-2004). Collision avoidance for satellites in formation flight. Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2, 1077-1093
Williams T.;Register J.;Slater G. (12-01-2004). Formation-keeping maneuver dispersions and safe mode insertion for satellite formation flight. Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 1, 1-19
Slater G. (12-01-2003). Cooperation between UAVs in a search and destroy mission. AIAA Guidance, Navigation, and Control Conference and Exhibit
Slater G. (12-01-2002). Adaptive improvement of aircraft climb performance for air traffic control applications. IEEE International Symposium on Intelligent Control - Proceedings, 602-607
Slater G. (01-01-2002). Delay distribution in a multi-center/multi-sector environment. AIAA Guidance, Navigation, and Control Conference and Exhibit
Slater G. (01-01-2002). Dynamics of self-spacing in a stream of in-trail aircraft. AIAA Guidance, Navigation, and Control Conference and Exhibit
Bolender M.; Slater G. (12-01-2000). Analysis and optimization of departure sequences. AIAA Guidance, Navigation, and Control Conference and Exhibit
Bolender M.A.;Slater G.L. (01-01-2000). Cost analysis of the departure - En route merge problem. Journal of Aircraft, 37 (1) , 23-29More Information
Bolender M.A.;Slater G.L.;Bolender M.A.;Slater G.L. (01-01-2000). Evaluation of scheduling methods for multiple runways. Journal of Aircraft, 37 (3) , 410-416More Information
Bolender M.A.;Slater G.L. (01-01-1999). Cost analysis of the departure-en route merge problem. 1999 Guidance, Navigation, and Control Conference and Exhibit, 1815-1825
Lambrecht M.;Slater G. (01-01-1999). Departure trajectory modeling for air traffic control automation tools. 1999 Guidance, Navigation, and Control Conference and Exhibit, 1507-1520
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
Bolender M.A.;Slater G.L. (01-01-1997). Departure trajectory synthesis and the intercept problem. 1997 Guidance, Navigation, and Control Conference, 444-454
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
Bolender M.A.;Slater G.L. (01-01-1996). Evaluation of scheduling methods for multiple runways. 1996 Guidance, Navigation, and Control Conference and Exhibit, 1-11
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
Bosse A.;Slater G. (12-01-1993). Identification of flexible space structure models using operating data. Proceedings of SPIE - The International Society for Optical Engineering, 1923 (pt 2) , 1437-1446
Dumbacher S.;Brown D.;Slater G. (12-01-1993). Arrayed transducers for rotating equipment component signature enhancement. Proceedings of SPIE - The International Society for Optical Engineering, 1923 (pt 1) , 545-554
Shelley S.;Allemang R.;Slater G.;Schultze J. (12-01-1993). Active vibration control utilizing an adaptive modal filter based modal control method. Proceedings of SPIE - The International Society for Optical Engineering, 1923 (pt 1) , 751-758
McLaren M.;Slater G. (06-01-1993). A disturbance model for control/structure optimization with output feedback control. Structural Optimization, 6 (2) , 123-133More Information
Livneh R.;Slater G. (01-01-1993). Simple Adaptive Controller with Applications to Wing Flutter. Control and Dynamic Systems, 57 (C) , 423-477More Information
Slater G.;McLaren M. (01-01-1993). Disturbance model for control/structure optimization with full statefeedback. Journal of Guidance, Control, and Dynamics, 16 (3) , 523-533More Information
Slater G.;Bosse A.;Zhang Q. (01-01-1992). Robustness of positive real controllers for large space structures. Journal of Guidance, Control, and Dynamics, 15 (1) , 58-64More Information
Livneh R.;Slater G. (01-01-1991). Adaptive controller for wing flutter with unmeasurable excitations and unmodelled dynamics. International Journal of Control, 53 (2) , 293-309More Information
McLaren M.;Slater G. (12-01-1990). Covariance approach to integrated control/structure optimization., 189-205
Slater G.L.;Zhang Q. (12-01-1990). Controller design by eigenspace assignment., 19-31
Livneh R.;Slater G. (12-01-1990). On the uniqueness of the simple adaptive controller gains., 726-730
Livneh R.;Slater G. (12-01-1990). Some conditions for strictly positive real and almost strictly positive real structures., 81-85
Livnch R.;McLaren M.D.;Slater G.L. (12-01-1990). Some conditions for almost strict positive realness. Proceedings of the IEEE Conference on Decision and Control, 4, 2512-2517
Slater G.L.;Bosse A.;Zhang Q. (12-01-1990). Practical experience with multivariable positivity controllers. Proceedings of the American Control Conference, 1445-1448
Zhang Q.;Slater G. (01-01-1990). Eigenstructure assignment with control gains optimization. Optimal Control Applications and Methods, 11 (2) , 127-141More Information
Slater G.;McLareir M. (01-01-1990). Estimator eigenvalue placement in positive real control. Journal of Guidance, Control, and Dynamics, 13 (1) , 168-175More Information
Zhang Q.;Slater G.;Allemang R. (01-01-1990). Suppression of undesired inputs of linear systems by eigenspace assignment. Journal of Guidance, Control, and Dynamics, 13 (2) , 330-336More Information
Slater G.L.;Stoughton M. (07-01-1987). ON-LINE DETERMINATION OF OPTIMAL FLIGHT PATHS FOR HELICOPTERS. Journal of the American Helicopter Society, 32 (3) , 54-61
McLaren M.;Slater G. (01-01-1987). Robust multivariable control of large space structures using positivity. Journal of Guidance, Control, and Dynamics, 10 (4) , 393-400More Information
McLaren M.;Slater G. (01-01-1986). Robust multivariable control of large space structures using positivity. Astrodynamics Conference, 1986
Takahashi M.;Slater G. (01-01-1986). Design of a flutter mode controller using positive real feedback. Journal of Guidance, Control, and Dynamics, 9 (3) , 339-345More Information
Slater G.;Livneh R. (12-01-1985). SECOND ORDER ADAPTIVE CONTROLLER FOR WING FLUTTER CONTROL. AIAA Paper, 679-687
Slater G. (01-01-1984). Perturbation analysis of optimal integral controls. Journal of Dynamic Systems, Measurement and Control, Transactions of the ASME, 106 (1) , 114-116More Information
Slater G.;Kandadai R. (01-01-1984). Gain optimization with non?linear controls. Optimal Control Applications and Methods, 5 (3) , 207-219More Information
Slater G.;Erzberger H. (01-01-1984). Optimal short-range trajectories for helicopters. Journal of Guidance, Control, and Dynamics, 7 (4) , 393-400More Information
Takahashi M.;Slater G. (01-01-1984). DESIGN OF A FLUTTER MODE CONTROLLER USING POSITIVE REAL FEEDBACK. AIAA Paper, 246-253
Slater G.;Stoughton M. (01-01-1984). ON-LINE DETERMINATION OF OPTIMAL FLIGHT PATHS FOR HELICOPTERS. Annual Forum Proceedings - American Helicopter Society, 461-470
Erzberger H.; Slater G. (01-01-1983). OPTIMAL SHORT RANGE TRAJECTORIES FOR HELICOPTERS. AIAA Paper
Slater G.;Kandadai R. (01-01-1982). Gain Optimization with Nonlinear Controls. Proceedings of the American Control Conference, 1982-June, 650-655
Slater G.;Kandadai R. (12-01-1981). DIGITAL CONTROL FOR FLEXIBLE AIRCRAFT USING REDUCED ORDER MODELS., 1
Mendenhall S.;Slater G. (01-01-1980). MODEL FOR HELICOPTER GUIDANCE ON SPIRAL TRAJECTORIES. AIAA Paper, 62-71
Keskar D.;Slater G. (01-01-1979). Load factor response of digitally controlled aircraft. Journal of Guidance, Control, and Dynamics, 2 (3) , 247-251More Information
Slater G. (01-01-1976). A Transformation approach to the terminal control problem. AIAA Journal, 14 (9) , 1206-1209More Information
Slater G.;Wells W. (01-01-1973). Optimal evasive tactics against a proportional navigation missile with time delay. Journal of Spacecraft and Rockets, 10 (5) , 309-313More Information
Slater G.;Wells W. (01-01-1971). On the Reduction of Optimal Time-Delay Systems to Ordinary Ones. IEEE Transactions on Automatic Control, 17 (1) , 154-155More Information