| Reduced-order entry trajectory planning for acceleration guidance KD Mease, DT Chen, P Teufel, Schoenenberger Journal of Guidance, Control, and Dynamics 25 (2), 257-266, 2002 | 223 | 2002 |
| Design and evaluation of an acceleration guidance algorithm for entry A Saraf, JA Leavitt, DT Chen, KD Mease Journal of Spacecraft and Rockets 41 (6), 986-996, 2004 | 219 | 2004 |
| Entry trajectory tracking law via feedback linearization S Bharadwaj, AV Rao, KD Mease Journal of Guidance, Control, and Dynamics 21 (5), 726-732, 1998 | 173 | 1998 |
| Inverse quantum-mechanical control: A means for design and a test of intuition P Gross, H Singh, H Rabitz, K Mease, GM Huang Physical Review A 47 (6), 4593, 1993 | 144 | 1993 |
| Shuttle entry guidance revisited using nonlinear geometric methods KD Mease, JP Kremer Journal of Guidance, Control, and Dynamics 17 (6), 1350-1356, 1994 | 127 | 1994 |
| Feasible trajectory generation for atmospheric entry guidance JA Leavitt, KD Mease Journal of Guidance, Control, and Dynamics 30 (2), 473-481, 2007 | 119 | 2007 |
| Drag-based predictive tracking guidance for Mars precision landing KY Tu, MS Munir, KD Mease, DS Bayard Journal of Guidance, Control, and Dynamics 23 (4), 620-628, 2000 | 114 | 2000 |
| Distributed and boundarycontrol of the viscous burgers' equation HV Ly, KD Mease, ES Titi Numerical Functional Analysis and Optimization 18 (1-2), 143-188, 1997 | 105 | 1997 |
| Reachable and controllable sets for planetary entry and landing J Benito, KD Mease Journal of guidance, control, and dynamics 33 (3), 641-654, 2010 | 92 | 2010 |
| Competitive tracking of molecular objectives described by quantum mechanics Y Chen, P Gross, V Ramakrishna, H Rabitz, K Mease The Journal of chemical physics 102 (20), 8001-8010, 1995 | 86 | 1995 |
| Landing footprint computation for entry vehicles A Saraf, J Leavitt, M Ferch, K Mease AIAA Guidance, Navigation, and Control Conference and Exhibit, 4774, 2004 | 79 | 2004 |
| Minimum-fuel powered descent for mars pinpoint landing U Topcu, J Casoliva, KD Mease Journal of Spacecraft and Rockets 44 (2), 324-331, 2007 | 75 | 2007 |
| Geometry and inverse optimality in global attitude stabilization S Bharadwaj, M Osipchuk, KD Mease, FC Park Journal of Guidance, Control, and Dynamics 21 (6), 930-939, 1998 | 72 | 1998 |
| Optimization of aeroassisted orbital transfer-current status KD Mease Journal of the Astronautical Sciences 36, 7-33, 1988 | 71 | 1988 |
| Sliding mode observer for drag tracking in entry guidance S Talole, J Benito, K Mease AIAA Guidance, Navigation and Control Conference and Exhibit, 6851, 2007 | 64 | 2007 |
| Performance of evolved acceleration guidance logic for entry (EAGLE) J Leavitt, A Saraf, D Chen, K Mease AIAA guidance, navigation, and control conference and exhibit, 4456, 2002 | 64 | 2002 |
| Minimum-fuel aeroassisted coplanar orbit transfer using lift-modulation KD Mease, NX Vinh Journal of Guidance, Control, and Dynamics 8 (1), 134-141, 1985 | 61 | 1985 |
| Eigenvector approximate dichotomic basis method for solving hyper‐sensitive optimal control problems AV Rao, KD Mease Optimal Control Applications and Methods 21 (1), 1-19, 2000 | 59 | 2000 |
| Fuel efficient powered descent guidance for mars landing U Topcu, J Casoliva, K Mease AIAA guidance, navigation, and control conference and exhibit, 6286, 2005 | 58 | 2005 |
| Dichotomic basis approach to solving hyper-sensitive optimal control problems AV Rao, KD Mease Automatica 35 (4), 633-642, 1999 | 55 | 1999 |
Anil V. RaoProfessor, University of FloridaBestätigte E-Mail-Adresse bei ufl.edu
