Robust adaptive control E Lavretsky, KA Wise Robust and adaptive control: With aerospace applications, 317-353, 2012 | 1058 | 2012 |
Agile missile dynamics and control KA Wise, DJB Roy Journal of Guidance, Control, and Dynamics 21 (3), 441-449, 1998 | 206 | 1998 |
Flight testing of reconfigurable control law on the X-36 tailless aircraft JS Brinker, KA Wise Journal of Guidance, Control, and Dynamics 24 (5), 903-909, 2001 | 201 | 2001 |
Adaptive control of flight: theory, applications, and open problems KA Wise, E Lavretsky, N Hovakimyan 2006 American Control Conference, 6 pp., 2006 | 135 | 2006 |
Stability and flying qualities robustness of a dynamic inversion aircraft control law JS Brinker, KA Wise Journal of Guidance, Control, and Dynamics 19 (6), 1270-1277, 1996 | 133 | 1996 |
Reconfigurable flight control for a tailless advanced fighter aircraft J Brinker, K Wise Guidance, Navigation, and Control Conference and Exhibit, 4107, 1998 | 123 | 1998 |
Direct adaptive reconfigurable flight control for a tailless advanced fighter aircraft KA Wise, JS Brinker, AJ Calise, DF Enns, MR Elgersma, P Voulgaris International Journal of Robust and Nonlinear Control 9 (14), 999-1012, 1999 | 108 | 1999 |
ℒ 1 adaptive controller for tailless unstable aircraft in the presence of unknown actuator failures VV Patel, C Cao, N Hovakimyan, KA Wise, E Lavretsky International Journal of Control 82 (4), 705-720, 2009 | 85 | 2009 |
Comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamics KA Wise Journal of Guidance, Control, and Dynamics 15 (4), 861-870, 1992 | 69 | 1992 |
Nonlinear H-infinity optimal control for agile missiles KA Wise, JL Sedwick Journal of guidance, control, and dynamics 19 (1), 157-165, 1996 | 58* | 1996 |
Application and flight testing of an adaptive autopilot on precision guided munitions M Sharma, E Lavretsky, K Wise AIAA Guidance, Navigation, and Control Conference and Exhibit, 6568, 2006 | 56 | 2006 |
Bank-to-turn missile autopilot design using loop transfer recovery KA Wise Journal of Guidance, control, and Dynamics 13 (1), 145-152, 1990 | 54 | 1990 |
Flight testing of the X-45A J-UCAS computational alpha-beta system K Wise AIAA Guidance, Navigation, and Control Conference and Exhibit, 6215, 2006 | 50 | 2006 |
Filter Design for Feedback-loop Trade-off of L_1 Adaptive Controller: A Linear Matrix Inequality Approach D Li, N Hovakimyan, C Cao, K Wise AIAA Guidance, Navigation and Control Conference and Exhibit, 6280, 2008 | 47 | 2008 |
Adaptive flight control of a sensor guided munition K Wise, E Lavretsky, J Zimmerman, J Francis, D Dixon, B Whitehead AIAA Guidance, Navigation, and Control Conference and Exhibit, 6385, 2005 | 44 | 2005 |
Singular value robustness tests for missile autopilot uncertainties KA Wise Journal of guidance, control, and dynamics 14 (3), 597-606, 1991 | 44 | 1991 |
L1 adaptive controller for air-breathing hypersonic vehicle with flexible body dynamics Y Lei, C Cao, E Cliff, N Hovakimyan, A Kurdila, K Wise 2009 American Control Conference, 3166-3171, 2009 | 42 | 2009 |
L1 adaptive controller for tailless unstable aircraft VV Patel, C Cao, N Hovakimyan, KA Wise, E Lavretsky 2007 American Control Conference, 5272-5277, 2007 | 42 | 2007 |
Computational air data system for angle-of-attack and angle-of-sideslip KA Wise US Patent 6,928,341, 2005 | 40 | 2005 |
Missile autopilot design using H∞optimal control with μ-synthesis KA Wise, BC Mears, K Poolia 1990 American Control Conference, 2362-2367, 1990 | 39 | 1990 |