Year |
Citation |
Score |
2018 |
Kang C, Cranford J, Sridhar MK, Kodali D, Landrum DB, Slegers N. Experimental Characterization of a Butterfly in Climbing Flight Aiaa Journal. 56: 15-24. DOI: 10.2514/1.J055360 |
0.316 |
|
2017 |
Cacan M, Scheuermann E, Ward M, Costello M, Slegers N. Utilizing ground-based LIDAR measurements to aid autonomous airdrop systems Journal of Aerospace Engineering. 231: 1763-1778. DOI: 10.1177/0954410017705402 |
0.301 |
|
2016 |
Slegers N, Heilman M, Cranford J, Lang A, Yoder J, Habegger M. Beneficial aerodynamic effect of wing scales on the climbing flight of butterflies. Bioinspiration & Biomimetics. PMID 28000615 DOI: 10.1088/1748-3190/Aa551D |
0.36 |
|
2015 |
Cacan MR, Scheuermann E, Ward M, Costello M, Slegers N. Autonomous Airdrop Systems Employing Ground Wind Measurements for Improved Landing Accuracy Ieee/Asme Transactions On Mechatronics. DOI: 10.1109/Tmech.2015.2405851 |
0.36 |
|
2015 |
Slegers N, Brown A, Rogers J. Experimental investigation of stochastic parafoil guidance using a graphics processing unit Aerodynamic Decelerator Systems Technology Conferences. DOI: 10.1016/J.Conengprac.2014.12.002 |
0.383 |
|
2014 |
Oduyela A, Slegers N. Gust mitigation of micro air vehicles using passive articulated wings. Thescientificworldjournal. 2014: 598523. PMID 24516368 DOI: 10.1155/2014/598523 |
0.414 |
|
2014 |
Orr JS, Slegers NJ. High-efficiency thrust vector control allocation Journal of Guidance, Control, and Dynamics. 37: 374-382. DOI: 10.2514/1.61644 |
0.56 |
|
2013 |
Kaviratna L, Costello M, Slegers N. Projectile fire-control algorithm in a spatially varying wind field Journal of Aerospace Information Systems. 10: 497-512. DOI: 10.2514/1.I010068 |
0.316 |
|
2012 |
Gorman CM, Slegers NJ. Evaluation of multibody parafoil dynamics using distributed miniature wireless sensors Journal of Aircraft. 49: 546-555. DOI: 10.2514/1.C031566 |
0.66 |
|
2012 |
Rogers J, Slegers N. Robust parafoil terminal guidance using massively parallel processing Aiaa Atmospheric Flight Mechanics Conference 2012. DOI: 10.2514/1.59782 |
0.351 |
|
2012 |
Ward M, Costello M, Slegers N. Specialized system identification for parafoil and payload systems Journal of Guidance, Control, and Dynamics. 35: 588-597. DOI: 10.2514/1.53364 |
0.444 |
|
2012 |
Rogers J, Slegers N, Costello M. A method for defining wind turbine setback standards Wind Energy. 15: 289-303. DOI: 10.1002/We.468 |
0.355 |
|
2011 |
Hembree B, Slegers N. Tethered aerostat modeling using an efficient recursive rigid-body dynamics approach Journal of Aircraft. 48: 623-632. DOI: 10.2514/1.C031179 |
0.322 |
|
2011 |
Slegers N, Yakimenko OA. Terminal guidance of autonomous parafoils in high wind-to-airspeed ratios Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 225: 336-346. DOI: 10.1243/09544100Jaero749 |
0.319 |
|
2011 |
Gorman CM, Slegers NJ. Evaluation of multi-body parafoil dynamics using distributed miniature wireless sensors Aiaa Atmospheric Flight Mechanics Conference 2011. |
0.659 |
|
2011 |
Gorman CM, Slegers NJ. Modeling of parafoil-payload relative yawing motion on autonomous parafoils 21st Aiaa Aerodynamic Decelerator Systems Technology Conference and Seminar 2011. |
0.655 |
|
2011 |
Gorman CM, Slegers NJ. Comparison and analysis of multi-body parafoil models with varying degrees of freedom 21st Aiaa Aerodynamic Decelerator Systems Technology Conference and Seminar 2011. |
0.686 |
|
2010 |
Hembree B, Slegers N. Tethered aerostat modeling using an efficient recursive rigid body dynamics approach Aiaa Atmospheric Flight Mechanics Conference 2010. DOI: 10.2514/1.C031179 |
0.424 |
|
2010 |
Ward M, Costello M, Slegers N. On the benefits of in-flight system identification for autonomous airdrop systems Journal of Guidance, Control, and Dynamics. 33: 1313-1326. DOI: 10.2514/1.49030 |
0.45 |
|
2009 |
Slegers N, Rogers J, Costello M, Puga M, Arons P. Modeling the risk of a failed wind turbine blade impacting a power transmission line Wind Engineering. 33: 587-606. DOI: 10.1260/0309-524X.33.6.587 |
0.322 |
|
2009 |
Harris J, Slegers N. Performance of a fire-and-forget anti-tank missile with a damaged wing Mathematical and Computer Modelling. 50: 292-305. DOI: 10.1016/J.Mcm.2009.02.009 |
0.409 |
|
2009 |
Slegers NJ, Yakimenko OA. Optimal control for terminal guidance of autonomous parafoils 20th Aiaa Aerodynamic Decelerator Systems Technology Conference. |
0.351 |
|
2009 |
Ward M, Costello M, Slegers N. Real-time system identification for an adaptive MPC autonomous airdrop system 20th Aiaa Aerodynamic Decelerator Systems Technology Conference. |
0.36 |
|
2009 |
Slegers NJ. Effects of canopy-payload relative motion on control of autonomous parafoils 20th Aiaa Aerodynamic Decelerator Systems Technology Conference. |
0.368 |
|
2008 |
Slegers N. Predictive control of a munition using low-speed linear theory Journal of Guidance, Control, and Dynamics. 31: 768-775. DOI: 10.2514/1.34329 |
0.381 |
|
2008 |
Slegers N, Beyer E, Costello M. Use of variable incidence angle for glide slope control of autonomous parafoils Journal of Guidance, Control, and Dynamics. 31: 585-596. DOI: 10.2514/1.32099 |
0.409 |
|
2007 |
Slegers N, Costello M. Variable structure observer for control bias on unmanned air vehicles Journal of Guidance, Control, and Dynamics. 30: 281-286. DOI: 10.2514/1.25321 |
0.394 |
|
2007 |
Slegers N, Beyer E, Costello M. Use of dynamic incidence angle for glide slope control of autonomous parafoils Collection of Technical Papers - 19th Aiaa Aerodynamic Decelerator Systems Technology Conference and Seminar. 217-243. |
0.32 |
|
2006 |
Slegers N, Kyle J, Costello M. Nonlinear model predictive control technique for unmanned air vehicles Journal of Guidance, Control, and Dynamics. 29: 1179-1188. DOI: 10.2514/1.21531 |
0.446 |
|
2005 |
Slegers N, Costello M. Model predictive control of a parafoil and payload system Journal of Guidance, Control, and Dynamics. 28: 816-821. DOI: 10.2514/1.12251 |
0.406 |
|
2003 |
Slegers N, Costello M. Aspects of Control for a Parafoil and Payload System Journal of Guidance, Control, and Dynamics. 26: 898-905. DOI: 10.2514/2.6933 |
0.38 |
|
2003 |
Slegers N, Costello M. Comparison of measured and simulated motion of a controllable parafoil and payload system Aiaa Atmospheric Flight Mechanics Conference and Exhibit. |
0.391 |
|
2003 |
Slegers N, Costello M. On the use of rigging angle and canopy tilt for control of a parafoil and payload system Aiaa Atmospheric Flight Mechanics Conference and Exhibit. |
0.305 |
|
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