Dr. Kevin A.Wise - Adjunct Professor
Journal Publications:
Direct Adaptive Reconfigurable Flight Control For A Tailless Advanced Fighter Aircraft, Int. Journal of Robust Nonlinear Control, to appear in 1999 (With J. Brinker, A. Calise, D. Enns, M Elgersma, and P. Voulgaris).
Affordable Flight Control For Aircraft and Missiles, contributed chapter in Perspectives in Control: New Concepts and Applications, IEEE Press, to appear 1999.
Agile Missile Dynamics and Control, Journal of Guidance, Control, and Dynamics, Vol. 21, No. 3, 1998, pp. 441-449. (With D. Broy)
Fighter Aircraft Control Challenges and Technology Transition, Systems and Control in the Twenty-First Century, Birkhauser, 1996.
Stability and Flying Qualities Robustness of a Dynamic Inversion Aircraft Control Law, Journal of Guidance, Control, and Dynamics, Vol. 19, No. 6, 1996, pp. 1270-1278. (With J. Brinker)
Nonlinear H-Infinity Optimal Control For Agile Missiles, Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, 1996, pp. 157-165. (With J. Sedwick)
Linear Quadratic Flight Control For Ejection Seats, Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, 1996, pp. 15-22. (With J. Brinker)
Missile Autopilot Robustness Using The Real Multiloop Stability Margin, Journal of Guidance, Control, and Dynamics, Vol. 16, No. 2, 1993, pp. 354-362.
A Comparison of Six Robustness Tests Evaluating Missile Autopilot Robustness To Uncertain Aerodynamics, Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 861-870.
Singular Value Robustness Tests For Missile Autopilot Uncertainties, Journal of Guidance, Control, and Dynamics, Vol. 14, No. 3, 1991, pp. 597-606.
Missile Autopilot Robustness To Uncertain Aerodynamics: Stability Hypersphere Radius Calculation, Vol. 14, No. 1, 1991, pp. 166-175.
Bank-To-Turn Missile Autopilot Design Using Loop Transfer Recovery, Journal of Guidance, Control, and Dynamics, Vol. 13, No. 1, 1990, pp. 145-152.
Conference Publications:
Nonlinear Simulation Analysis of a Tailless Advanced Fighter Aircraft Reconfigurable Flight Control Law, to be published in the Proc. of the AIAA GNC Conference, Portland, OR, August, 1999, (with J. Brinker)
Reconfigurable Flight Control for a Tailless Advanced Fighter Aircraft, Proc. of the AIAA GNC Conference, Boston, MA, August, 1998, pp. 75-87, (with J. Brinker)
Stability Analysis of Reconfigurable and Gain Scheduled Flight Control Systems Using LMIs, Proc. of the AIAA GNC Conference, Boston, MA, August, 1998, pp.118-126 (with J. Sedwick)
Nonlinear Control Of Agile Missiles Using State Dependent Riccati Equations, Proc. Of the 1997 ACC, Albuquerque NM, June 1997, pp. 379-380. (With J. Sedwick)
Agile Missile Dynamics and Control, AIAA paper No. 96-3912, presented at the AIAA GNC Conference, San Diego CA, August 1996. (With D. Broy),
Applied Control Research Topics in the Aerospace Industry, Proc. of the 34th IEEE CDC, New Orleans LA, Dec. 1995, pp. 751-756.
Nonlinear H¥ Optimal Control For Agile Missiles, Proc of the 1995 AIAA GNC Conference, Balt. MD, Aug. 1995, pp. 1295-1307. (With J. Sedwick)
Linear Quadratic Flight Control For Ejection Seats, Proc of the 1995 AIAA GNC Conference, Balt. MD, Aug. 1995, pp. 1325-1337. (With J. Brinker)
Successive Approximation Solution to the Hamilton-Jacobi-Isaacs Equation, Proc of the 33rd IEEE CDC, Orlando FL, Dec. 1994, pp. 1387-1391. (With J. Sedwick).
Missile Autopilot Design Using Nonlinear H¥ Optimal Control, Proc. of the 13th IFAC Symposium Automatic Control In Aerospace, Palo Alto CA, Sept. 1994, pp. 128-134. (With J. Sedwick)
Flight Control For The Fourth Generation Escape System Program, Presented at the 1994 SAFE Conference, Reno NV, Oct. 1994. (With J. Ritland and J. Brinker)
H¥ Missile Autopilot Design With and Without Imaginary Axis Zeros, Proc. of the ACC, Baltimore MD, June 1994, pp. 1670-1674. (With E. Hamby)
A Parameter Space Robustness Test for Real and Complex Uncertainties, Proc. of the 32nd IEEE CDC, San Antonio, TX, Dec. 13-17, 1993.
High Gain H¥ Feedback Control for an Anti-Air Missile, Proc. of the 32nd IEEE CDC, San Antonio, TX, Dec. 13-17, 1993. (with R. Eberhardt)
Missile Autopilot Robustness To Real and Complex Uncertainties Using A Parameter Space Robustness Test, Proceedings of the AIAA Guidance, Navigation, and Control Conference, Monterey, CA, August, 1993, Paper AIAA 93-3738, pp. 336-346 (with K. Reddy).
TVC Control for the AIAA Controls Design Airplane, Proceedings of the AIAA Guidance, Navigation, and Control Conference, Monterey, CA, August, 1993, Paper AIAA 93-3810, pp. 995-1005 (with M. Dierks).
Linear and Nonlinear Aircraft Flight Control for the AIAA Controls Design Challenge, Presented at the AIAA Guidance, Navigation, and Control Conference, Hilton Head, SC, August, 1992, Paper AIAA 92-4628, (with M. Dierks, B. Kerkemeyer, J. Tang).
Nonlinear Aircraft Flight Control Using Dynamic Inversion, Proc of the American Control Conference, Chicago, IL, June, 1992.
Automated Gain Schedules for Missile Autopilots Using Robustness Theory, Proc. of the First IEEE Conference on Control Applications, Dayton, OH, May, 1992 (with R. Eberhardt).
Optimal Disturbance Rejection In Missile Autopilot design Using Projective Controls, Proc. of the 30th IEEE CDC, Brighton, UK, Dec. 11-13, 1991 (with T. Nguyen).
Blended Aero & Reaction Jet Missile Autopilot Design Using VSS Techniques, Proc. of the 30th IEEE CDC, Brighton, UK, Dec. 11-13, 1991 (with R. Weil).
Approximating a Linear Quadratic Missile Autopilot Design Using an Output Feedback Projective Control, Proceedings of the AIAA Guidance, Navigation, and Control Conference, New Orleans, LA, August, 1991, Paper AIAA 91-2613, pp. 114-122 (with F. Deylami).
Linear and Nonlinear Flight Control of the AIAA Design Challenge Airplane, Proceedings of the AIAA Guidance, Navigation, and Control Conference, New Orleans, LA, August, 1991, Paper AIAA 91-2634, pp. 308-318 (with A. Godhwani, K. Gu, M. Dierks, B. Kerkemeyer, J. Tang).
Linear and Nonlinear Controllers for Robust Stabilization Problems: A Survey, to appear in IFAC, 1990, Tallin, USSR, (with K. Poolla and J. Shamma).
Missile Autopilot Robustness Using The Multiloop Stability Margin, Proceedings of the AIAA Guidance, Navigation, and Control Conference, Portland, OR, August, 1990, Paper AIAA 90-3340, pp. 232-241.
A Convex Hull Program Evaluating Control System Robustness To Real Parameter Variations, Proceedings of the AIAA Guidance, Navigation, and Control Conference, Portland, OR, August, 1990, Paper AIAA 90-3339, pp. 223-231 (with B. Mears, C. Tang, A. Godhwani)
Missile Autopilot Design Using H• Optimal Control With µ-Synthesis, Proceedings of the American Control Conference, San Diego, CA. May, 1990, pp. 2362-2367, (with B. Mears and K. Poolla).
A Comparison of Six Robustness Tests Evaluating Missile Autopilot Robustness To Uncertain Aerodynamics, Proceedings of the American Control Conference, San Diego, CA. May, 1990, pp. 755-763.
Singular Value Robustness Tests For Missile Autopilot Uncertainties, Proceedings of the 1989 AIAA Guidance, Navigation, and Control Conference, Paper AIAA 89-3552, pp. 1079-1089.
Missile Autopilot Robustness To Uncertain Aerodynamics: Stability Hypersphere Radius Calculation, Proceedings of the 1989 AIAA Guidance, Navigation, and Control Conference, Paper AIAA 89-3553, pp. 1090-1099.
Maximizing Performance and Stability Robustness In A Conventional Bank-To-Turn Missile Autopilot Design, Proceedings of the 1988 Missile Systems Missile Sciences Conference, Monterey, CA., Paper AIAA-88-C-1036.
Optimizing Singular Value Robustness Measures In A Conventional Bank-To-Turn Missile Autopilot Design, Proceedings of the 1988 AIAA Guidance, Navigation, and Control Conference, AIAA Paper 88-4089, pp. 296-306.
A Bank-To-Turn Missile Autopilot Design Approach Using LQG/LTR Control Theory", Proceedings of the AIAA 26th Aerospace Sciences Meeting, Reno, Nevada, January, 1988.
Modeling and Identification of a Light Truck Engine Mounting System for Ride Quality Optimization", presented at the SAE International Off-Highway and Powerplant Congress, Milwaukee, Wisconsin. Published in the Transactions of the SAE. September 1984. (with R. Reid)
Comparison of Automatic Steering Performance of A VLCC in a Seaway Resulting from Application of LQG and Classical Control System Design Techniques", Proc., 6th Ship Control Systems Symp., Ottawa, Canada, October 1981. (with R. Reid, B. Mears, A. Tugcu, D. Griffin, and V. Williams)
