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 ) ,1585-1600 More 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 ) ,53-65 More 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 ) ,1140-1146 More 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 ) ,360-363 More 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 ) ,23-29 More 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 ) ,410-416 More 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 ) ,123-133 More Information
Livneh R.;Slater G. (01-01-1993. ) Simple Adaptive Controller with Applications to Wing Flutter.Control and Dynamic Systems, , 57 (C ) ,423-477 More 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 ) ,523-533 More 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 ) ,58-64 More 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 ) ,293-309 More 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 ) ,127-141 More Information
Slater G.;McLareir M. (01-01-1990. ) Estimator eigenvalue placement in positive real control.Journal of Guidance, Control, and Dynamics, , 13 (1 ) ,168-175 More 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 ) ,330-336 More 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 ) ,393-400 More 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 ) ,339-345 More 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 ) ,114-116 More Information
Slater G.;Kandadai R. (01-01-1984. ) Gain optimization with non?linear controls.Optimal Control Applications and Methods, , 5 (3 ) ,207-219 More Information
Slater G.;Erzberger H. (01-01-1984. ) Optimal short-range trajectories for helicopters.Journal of Guidance, Control, and Dynamics, , 7 (4 ) ,393-400 More 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 ) ,247-251 More Information
Slater G. (01-01-1976. ) A Transformation approach to the terminal control problem.AIAA Journal, , 14 (9 ) ,1206-1209 More 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 ) ,309-313 More 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 ) ,154-155 More Information