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Rick Lind - Publications

Affiliations: 
University of Florida, Gainesville, Gainesville, FL, United States 
Area:
Aerospace Engineering, Mechanical Engineering, Robotics Engineering
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66 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2015 Davis J, Kim NH, Lind R. Control of the Flexural Axis of a Wing with Piezoelectric Actuation Journal of Aircraft. 52: 584-594. DOI: 10.2514/1.C032776  0.432
2014 Babcock J, Lind R. Aeroelastic effects of battens on the flight dynamics of a MAV Aeronautical Journal. 118: 985-1008. DOI: 10.1017/S0001924000009714  0.746
2013 Chatterjee S, Lind R, Roberts B. The novel characteristics of pterosaurs: Biological inspiration for robotic vehicles International Journal of Design and Nature and Ecodynamics. 8: 113-143. DOI: 10.2495/Dne-V8-N2-113-143  0.399
2013 Pachikara AJ, Kehoe JJ, Lind R. Path-Parameterization Approach Using Trajectory Primitives for Three-Dimensional Motion Planning Journal of Aerospace Engineering. 26: 571-585. DOI: 10.1061/(Asce)As.1943-5525.0000152  0.302
2013 Babcock J, Lind R. Control synthesis for virtually changing wing stiffness Aiaa Atmospheric Flight Mechanics (Afm) Conference.  0.471
2013 Jorge A, Lind R. Control of a stochastic model of an aeroelastic micro air vehicle in turbulence Aiaa Atmospheric Flight Mechanics (Afm) Conference.  0.389
2012 Pachikara AJ, Lind R. Flight dynamics of a micro air vehicle with aeroservoelastic interactions across a range of wing stiffness Aiaa Atmospheric Flight Mechanics Conference 2012. DOI: 10.2514/6.2012-4577  0.469
2012 Carter R, Lind R. Parametric modeling for store separation aerodynamics using system identification Aiaa Atmospheric Flight Mechanics Conference 2012. DOI: 10.2514/6.2012-4510  0.303
2012 Babcock J, Lind R. Aeroelastic effects of wing stiffness on the flight dynamics of a MAV Aiaa Atmospheric Flight Mechanics Conference 2012. DOI: 10.2514/6.2012-4400  0.39
2012 Johnson B, Lind R. Trajectory planning for sensing effectiveness with high angle-of-attack flight capability 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-276  0.317
2012 Carter R, Lind R. Trajectory optimization for guided store separation Aiaa Guidance, Navigation, and Control Conference 2012.  0.312
2011 Roberts B, Lind R, Chatterjee S. Flight dynamics of a pterosaur-inspired aircraft utilizing a variable-placement vertical tail. Bioinspiration & Biomimetics. 6: 026010. PMID 21558603 DOI: 10.1088/1748-3182/6/2/026010  0.494
2011 Bhat S, Lind R. Control-oriented design using surrogate-based optimization and existence conditions for robust performance Aiaa Journal. 49: 2577-2581. DOI: 10.2514/1.J050700  0.668
2011 Love R, Lind R. Time-frequency analysis of aeroelastic deflections of flapping wings International Journal of Micro Air Vehicles. 3: 89-100. DOI: 10.1260/1756-8293.3.2.89  0.314
2011 Arvai AR, Kehoe JJ, Lind R. Vision-Based Navigation Using Multi-Rate Feedback From Optic Flow And Scene Reconstruction Aeronautical Journal. 115: 411-420. DOI: 10.1017/S0001924000006035  0.353
2010 Grant DT, Abdulrahim M, Lind R. Design and analysis of biomimetic joints for morphing of micro air vehicles. Bioinspiration & Biomimetics. 5: 045007. PMID 21098958 DOI: 10.1088/1748-3182/5/4/045007  0.775
2010 Bhat S, Lind R. Control-oriented design of operating range for linear parameter varying systems for closed-loop performance Aiaa Guidance, Navigation, and Control Conference. DOI: 10.2514/6.2010-8412  0.347
2010 Grant DT, Lind R. Optimal tracking of time-varying modes for control of morphing aircraft Aiaa Guidance, Navigation, and Control Conference. DOI: 10.2514/6.2010-8203  0.334
2010 Wilcox ZD, MacKunis W, Bhat S, Lind R, Dixon WE. Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects Journal of Guidance, Control, and Dynamics. 33: 1213-1224. DOI: 10.2514/1.46785  0.651
2010 Johnson B, Lind R. Characterizing wing rock with variations in size and configuration of vertical tail Journal of Aircraft. 47: 567-576. DOI: 10.2514/1.45719  0.366
2010 Chatterjee S, Roberts B, Lind R. Pterodrone: A pterodactyl-inspired unmanned air vehicle that flies, walks, climbs, and sails Wit Transactions On Ecology and the Environment. 138: 301-316. DOI: 10.2495/DN100261  0.388
2010 Grant DT, Abdulrahim M, Lind R. Flight Dynamics of a Morphing Aircraft Utilizing Independent Multiple-Joint Wing Sweep International Journal of Micro Air Vehicles. 2: 91-106. DOI: 10.1260/1756-8293.2.2.91  0.77
2010 Love R, Lind R. Experimentally-based aeroservoelastic system identification and feedforward control of flexible flapping wings Aiaa Atmospheric Flight Mechanics Conference 2010.  0.341
2009 Chakravarthy A, Grant DT, Lind R. Time-varying dynamics of a micro air vehicle with variable-sweep morphing Aiaa Guidance, Navigation, and Control Conference and Exhibit. DOI: 10.2514/1.55078  0.444
2009 Wright K, Lind R. Sensor emplacement on vertical surfaces with biologically inspired morphing from bats Journal of Aircraft. 46: 1450-1454. DOI: 10.2514/1.42859  0.38
2009 Lind R. Flutter margins for multi-mode unstable couplings with associated flutter confidence Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/1.40328  0.335
2009 Baldelli DH, Zeng J, Lind R, Harris C. Flutter-Prediction Tool for Flight-Test-Based Aeroelastic Parameter-Varying Models Journal of Guidance Control and Dynamics. 32: 158-171. DOI: 10.2514/1.36584  0.352
2009 Gans NR, Dixon WE, Lind R, Kurdila A. A hardware in the loop simulation platform for vision-based control of unmanned air vehicles Mechatronics. 19: 1043-1056. DOI: 10.1016/J.Mechatronics.2009.06.014  0.478
2009 Johnson B, Lind R. High angle-of-attack flight dynamics of small UAVs 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.  0.337
2009 Love R, Lind R. Identification of aeroservoelastic models from experimental flapping-wing deflections Aiaa Atmospheric Flight Mechanics Conference.  0.354
2009 Creagh MA, Lind R. H-infinity control for attitude manoeuvres of a spinning asymmetric vehicle Aiaa Guidance, Navigation, and Control Conference and Exhibit.  0.3
2008 Baldelli DH, Lind R, Brenner M. Control-oriented flutter/limit-cycle-oscillation prediction framework Journal of Guidance, Control, and Dynamics. 31: 1634-1643. DOI: 10.2514/1.36117  0.361
2007 Stanford B, Abdulrahim M, Lind R, Ifju P. Investigation of Membrane Actuation for Roll Control of a Micro Air Vehicle Journal of Aircraft. 44: 741-749. DOI: 10.2514/1.25356  0.771
2007 Xu Y, Fitz-Coy N, Lind R, Tatsch A. μ Control for Satellites Formation Flying Journal of Aerospace Engineering. 20: 10-21. DOI: 10.1061/(Asce)0893-1321(2007)20:1(10)  0.469
2007 Wright K, Lind R. Investigating sensor emplacement on vertical surfaces for a biologically-inspired morphing design from bats Collection of Technical Papers - 2007 Aiaa Atmospheric Flight Mechanics Conference. 1: 505-512.  0.315
2007 Grant DT, Lind R. Effects of time-varying inertias on flight dynamics of an asymmetric variable-sweep morphing aircraft Collection of Technical Papers - 2007 Aiaa Atmospheric Flight Mechanics Conference. 1: 490-504.  0.346
2006 Kehoe JJ, Causey RS, Abdulrahim M, Lind R. Waypoint navigation for a micro air vehicle using vision-based attitude estimation The Aeronautical Journal. 110: 821-829. DOI: 10.1017/S000192400000169X  0.743
2006 Abdulrahim M, Lind R. Modeling and control of micro air vehicles with biologically-inspired morphing Proceedings of the American Control Conference. 2006: 2718-2723.  0.462
2006 Abdulrahim M, Lind R. Using Avian morphology to enhance aircraft maneuverability Collection of Technical Papers - 2006 Atmospheric Flight Mechanics Conference. 2: 1328-1344.  0.754
2005 Abdulrahim M, Garcia H, Lind R. Flight characteristics of shaping the membrane wing of a micro air vehicle Journal of Aircraft. 42: 131-137. DOI: 10.2514/1.4782  0.767
2005 Lind R, Mortagua JP. Reducing conservatism in flutterometer predictions using volterra modeling with modal parameter estimation Journal of Aircraft. 42: 998-1004. DOI: 10.2514/1.3116  0.367
2005 Baldelli DH, Lind R, Brenner M. Nonlinear aeroelastic/aeroservoelastic modeling by block-oriented identification Journal of Guidance, Control, and Dynamics. 28: 1056-1064. DOI: 10.2514/1.11792  0.391
2005 Lind R, Prazenica RJ, Brenner MJ. Estimating Nonlinearity Using Volterra Kernels in Feedback with Linear Models Nonlinear Dynamics. 39: 3-23. DOI: 10.1007/S11071-005-1906-0  0.364
2005 Abdulrahim M, Lind R. Control and simulation of a multi-role morphing micro air vehicle Collection of Technical Papers - Aiaa Guidance, Navigation, and Control Conference. 8: 6408-6426.  0.77
2004 Abdulrahim M, Boothe K, Lind R, Ifju P. Flight Characterization of Micro Air Vehicles Using Morphing for Agility and Maneuvering Sae Transactions. 113: 1704-1712. DOI: 10.4271/2004-01-3138  0.749
2004 Kehoe JJ, Causey R, Lind R, Kurdila AJ. Maneuvering and Tracking for a Micro Air Vehicle Using Vision-Based Feedback Sae Transactions. 113: 1694-1703. DOI: 10.4271/2004-01-3137  0.459
2004 Albertani R, Hubner P, Ifju P, Lind R, Jackowski J. Wind Tunnel Testing of Micro Air Vehicles at Low Reynolds Numbers Sae Transactions. 113: 1474-1486. DOI: 10.4271/2004-01-3090  0.452
2004 Webb TP, Prazenica RJ, Kurdila AJ, Lind R. Vision-based state estimation for autonomous micro air vehicles Collection of Technical Papers - Aiaa Guidance, Navigation, and Control Conference. 5: 3111-3124. DOI: 10.2514/1.22398  0.462
2004 Lind R, Prazenica RJ, Brenner MJ, Baldelli DH. Identifying Parameter-Dependent Volterra Kernels to Predict Aeroelastic Instabilities Aiaa Journal. 43: 2496-2502. DOI: 10.2514/1.12042  0.348
2004 Abdulrahim M, Lind R. Flight testing and response characteristics of a variable gull-wing morphing aircraft Collection of Technical Papers - Aiaa Guidance, Navigation, and Control Conference. 3: 1664-1679.  0.449
2003 Lind R. Flight-test evaluation of flutter prediction methods Journal of Aircraft. 40: 964-970. DOI: 10.2514/2.6881  0.326
2003 Fitzpatrick K, Feng Y, Lind R, Kurdila AJ, Mikolaitis DW. Flow Control in a Driven Cavity Incorporating Excitation Phase Differential Journal of Guidance Control and Dynamics. 28: 63-70. DOI: 10.2514/1.4664  0.344
2003 Lind R, Voracek DF, Truax R, Doyle T, Potter S, Brenner M. A flight test to demonstrate flutter and evaluate the flutterometer Aeronautical Journal. 107: 577-588. DOI: 10.1017/S0001924000013798  0.343
2003 Abdulrahim M, Lind R. Investigating segmented trailing-edge surfaces for full authority control of a UAV Aiaa Atmospheric Flight Mechanics Conference and Exhibit.  0.736
2002 Lind R. Linear parameter-varying modeling and control of structural dynamics with aerothermoelastic effects Journal of Guidance, Control, and Dynamics. 25: 733-739. DOI: 10.2514/2.4940  0.454
2002 Lind R. Match-point solutions for robust flutter analysis Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 1: 688-698. DOI: 10.2514/2.2900  0.349
2001 Lind R. Flight testing with the flutterometer 19th Aiaa Applied Aerodynamics Conference. DOI: 10.2514/2.3132  0.37
2000 Lind R, Brenner M. Flutterometer: an on-line tool to predict robust flutter margins Journal of Aircraft. 37: 1105-1112. DOI: 10.2514/2.2719  0.375
2000 Lind R, Burken JJ. μ-synthesis of an F/A-18 controller Aiaa Guidance, Navigation, and Control Conference and Exhibit.  0.33
1999 Lind R. Gain-sgheduled approximations to controllers H∞ for the F/A-18 active aeroelastic wing 1999 Guidance, Navigation, and Control Conference and Exhibit. 1220-1230.  0.313
1999 Lind R, Bumngton JR, Sparks AK. Multi-loop aeroservoelastic control of a hypersonic vehicle 1999 Guidance, Navigation, and Control Conference and Exhibit. 872-882.  0.382
1998 Lind R, Freudinger LC, Voracek DF. Comparison of Aeroelastic Excitation Mechanisms Journal of Aircraft. 35: 830-832. DOI: 10.2514/2.7585  0.34
1998 Brenner M, Lind R. Wavelet-processed flight data for robust aeroservoelastic stability margins Journal of Guidance, Control, and Dynamics. 21: 823-829. DOI: 10.2514/2.4331  0.376
1998 Lind R, Brenner M. Incorporating flight data into a robust aeroelastic model Journal of Aircraft. 35: 470-477. DOI: 10.2514/2.2320  0.421
1997 Lind R, Brenner M. Robust flutter margins of an F/A-18 aircraft from aeroelastic flight data Journal of Guidance, Control, and Dynamics. 20: 597-604. DOI: 10.2514/2.4082  0.408
1996 Balas GJ, Lind R, Packard A. Optimally scaled H-infinity full information control synthesis with real uncertainty Journal of Guidance Control and Dynamics. 19: 854-862. DOI: 10.2514/3.21710  0.372
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