| Year |
Citation |
Score |
| 2015 |
Sanabria DE, Balas G, Arndt R. Modeling, Control, and Experimental Validation of a High-Speed Supercavitating Vehicle Ieee Journal of Oceanic Engineering. 40: 362-373. DOI: 10.1109/Joe.2014.2312591 |
0.508 |
|
| 2015 |
Moreno CP, Pfifer H, Balas GJ. Actuator and sensor selection for robust control of aeroservoelastic systems Proceedings of the American Control Conference. 2015: 1899-1904. DOI: 10.1109/ACC.2015.7171010 |
0.306 |
|
| 2014 |
Dorobantu A, Balas GJ, Georgiou TT. Validating aircraft models in the gap metric Journal of Aircraft. 51: 1665-1672. DOI: 10.2514/1.C032580 |
0.79 |
|
| 2014 |
Moreno CP, Seiler PJ, Balas GJ. Model reduction for aeroservoelastic systems Journal of Aircraft. 51: 280-290. DOI: 10.2514/1.C032341 |
0.43 |
|
| 2014 |
Rosa P, Balas GJ, Silvestre C, Athans M. A synthesis method of LTI MIMO robust controllers for uncertain LPV plants Ieee Transactions On Automatic Control. 59: 2234-2240. DOI: 10.1109/Tac.2014.2301572 |
0.464 |
|
| 2014 |
Balas G. IEEE Control Systems Society Outreach Fund [Member Activities] Ieee Control Systems Magazine. 34: 18-20. DOI: 10.1109/Mcs.2013.2285297 |
0.375 |
|
| 2014 |
Escobar Sanabria D, Balas GJ, Arndt REA. Planing avoidance control for supercavitating vehicles Proceedings of the American Control Conference. 4979-4984. DOI: 10.1109/ACC.2014.6859485 |
0.399 |
|
| 2014 |
Freeman P, Balas GJ. Actuation failure modes and effects analysis for a small UAV Proceedings of the American Control Conference. 1292-1297. DOI: 10.1109/ACC.2014.6859482 |
0.329 |
|
| 2014 |
Hjartarson A, Seiler P, Balas GJ. LPV analysis of a gain scheduled control for an aeroelastic aircraft Proceedings of the American Control Conference. 3778-3783. DOI: 10.1109/ACC.2014.6859301 |
0.815 |
|
| 2014 |
Edwards C, Marcos A, Balas G. Special issue on linear parameter varying systems International Journal of Robust and Nonlinear Control. 24: 1925-1926. DOI: 10.1002/Rnc.3228 |
0.358 |
|
| 2014 |
Vanek B, Balas GJ, Arndt REA. Linear Parameter Varying control of the supercavitating vehicle 2009 European Control Conference, Ecc 2009. 2614-2621. |
0.747 |
|
| 2014 |
Rosa P, Balas GJ, Silvestre C, Athans M. On the synthesis of robust multiple-model adaptive controllers (RMMAC) using BMI/LPV controllers 2009 European Control Conference, Ecc 2009. 1644-1649. |
0.422 |
|
| 2013 |
Dorobantu A, Murch A, Mettler B, Balas G. System identification for small, low-cost, fixed-wing unmanned aircraft Journal of Aircraft. 50: 1117-1130. DOI: 10.2514/1.C032065 |
0.774 |
|
| 2013 |
Freeman P, Pandita R, Srivastava N, Balas GJ. Model-based and data-driven fault detection performance for a small UAV Ieee/Asme Transactions On Mechatronics. 18: 1300-1309. DOI: 10.1109/Tmech.2013.2258678 |
0.75 |
|
| 2013 |
Ozdemir AA, Seiler P, Balas GJ. Design tradeoffs of wind turbine preview control Ieee Transactions On Control Systems Technology. 21: 1143-1154. DOI: 10.1109/Tcst.2013.2261069 |
0.693 |
|
| 2013 |
Freeman P, Seiler P, Balas GJ. Air data system fault modeling and detection Control Engineering Practice. 21: 1290-1301. DOI: 10.1016/J.Conengprac.2013.05.007 |
0.691 |
|
| 2013 |
Summers E, Chakraborty A, Tan W, Topcu U, Seiler PJ, Balas G, Packard A. Quantitative local L2-gain and Reachability analysis for nonlinear systems International Journal of Robust and Nonlinear Control. 23: 1115-1135. DOI: 10.1002/Rnc.2948 |
0.573 |
|
| 2013 |
Pandita R, Bokor J, Balas G. Closed-loop performance metrics for fault detection and isolation filter and controller interaction International Journal of Robust and Nonlinear Control. 23: 419-438. DOI: 10.1002/Rnc.1838 |
0.628 |
|
| 2013 |
Dorobantu A, Seiler PJ, Balas GJ. Validating uncertain aircraft simulation models using flight test data Aiaa Atmospheric Flight Mechanics (Afm) Conference. |
0.792 |
|
| 2013 |
Hjartarson A, Seiler PJ, Balas GJ. LPV aeroservoelastic control using the LPVTools toolbox Aiaa Atmospheric Flight Mechanics (Afm) Conference. |
0.783 |
|
| 2013 |
Ozdemir AA, Seilery P, Balas GJ. Benefits of preview wind information for region 2 wind turbine control 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.572 |
|
| 2012 |
Moreno CP, Seiler P, Balas GJ. Linear, parameter varying model reduction for aeroservoelastic systems Aiaa Atmospheric Flight Mechanics Conference 2012. DOI: 10.2514/6.2012-4859 |
0.321 |
|
| 2012 |
Ozdemir AA, Seiler P, Balas GJ. Fundamental limitations of preview for wind turbine control 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. DOI: 10.2514/6.2012-1023 |
0.646 |
|
| 2012 |
Dorobantu A, Seiler P, Balas GJ. Time-delay margin analysis for an adaptive controller Journal of Guidance, Control, and Dynamics. 35: 1418-1425. DOI: 10.2514/1.56719 |
0.825 |
|
| 2012 |
Mokhtarzadeh H, Balas G, Arndt R. Effect of Cavitator on Supercavitating Vehicle Dynamics Ieee Journal of Oceanic Engineering. 37: 156-165. DOI: 10.1109/Joe.2011.2177689 |
0.416 |
|
| 2012 |
Seiler P, Balas GJ, Packard AK. Assessment of aircraft flight controllers using nonlinear robustness analysis techniques Lecture Notes in Control and Information Sciences. 416: 369-397. DOI: 10.1007/978-3-642-22627-4_19 |
0.35 |
|
| 2012 |
Seiler P, Balas GJ, Packard A. Linear parameter-varying control for the X-53 active aeroelastic wing Control of Linear Parameter Varying Systems With Applications. 2147483647: 483-512. DOI: 10.1007/978-1-4614-1833-7_19 |
0.526 |
|
| 2012 |
Balas GJ. Fault tolerant control and fault detection/isolation design for linear parameter varying systems International Journal of Adaptive Control and Signal Processing. 26: 189. DOI: 10.1002/Acs.2276 |
0.353 |
|
| 2012 |
Dorobantu A, Murch AM, Balas GJ. H ∞ robust control design for the NASA AirSTAR flight test vehicle 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.807 |
|
| 2012 |
Balas GJ, Moreno C, Seiler PJ. Robust aeroservoelastic control utilizing physics-based aerodynamic sensing Aiaa Guidance, Navigation, and Control Conference 2012. |
0.397 |
|
| 2012 |
Seiler P, Ozdemir AA, Balas GJ. Performance limits with preview information and actuator rate constraints Proceedings of the American Control Conference. 5532-5537. |
0.615 |
|
| 2011 |
Freeman P, Seiler P, Balas GJ. Robust fault detection for commercial transport air data probes Ifac Proceedings Volumes (Ifac-Papersonline). 18: 13723-13728. DOI: 10.3182/20110828-6-It-1002.03750 |
0.686 |
|
| 2011 |
Vanek B, Seiler P, Bokor J, Balas GJ. Robust model matching for geometric fault detection filters: a commercial aircraft example Ifac Proceedings Volumes (Ifac-Papersonline). 18: 7256-7261. DOI: 10.3182/20110828-6-It-1002.03440 |
0.691 |
|
| 2011 |
Ozdemir AA, Seiler P, Balas GJ. Wind turbine fault detection using counter-based residual thresholding Ifac Proceedings Volumes (Ifac-Papersonline). 18: 8289-8294. DOI: 10.3182/20110828-6-It-1002.01758 |
0.586 |
|
| 2011 |
Chakraborty A, Seiler P, Balas GJ. Susceptibility of F/A-18 flight controllers to the falling-leaf mode: Nonlinear analysis Journal of Guidance, Control, and Dynamics. 34: 73-85. DOI: 10.2514/1.50674 |
0.632 |
|
| 2011 |
Chakraborty A, Seiler P, Balas GJ. Susceptibility of F/A-18 flight controllers to the falling-leaf mode: Linear analysis Journal of Guidance, Control, and Dynamics. 34: 57-72. DOI: 10.2514/1.50674 |
0.367 |
|
| 2011 |
Ozdemir AA, Seiler PJ, Balas GJ. Performance of disturbance augmented control design in turbulent wind conditions Mechatronics. 21: 634-644. DOI: 10.1016/J.Mechatronics.2011.01.008 |
0.633 |
|
| 2011 |
Paw YC, Balas GJ. Development and application of an integrated framework for small UAV flight control development Mechatronics. 21: 789-802. DOI: 10.1016/J.Mechatronics.2010.09.009 |
0.828 |
|
| 2011 |
Chakraborty A, Seiler P, Balas GJ. Nonlinear region of attraction analysis for flight control verification and validation Control Engineering Practice. 19: 335-345. DOI: 10.1016/J.Conengprac.2010.12.001 |
0.628 |
|
| 2011 |
Dorobantu A, Seller PJ, Balas GJ. Time delay margin analysis applied to model reference adaptive control Aiaa Guidance, Navigation, and Control Conference 2011. |
0.817 |
|
| 2011 |
Dorobantu A, Murch AM, Mettler B, Balas GJ. Frequency domain system identification for a small, low-cost, fixed-wing UAV Aiaa Guidance, Navigation, and Control Conference 2011. |
0.768 |
|
| 2011 |
Seiler P, Balas GJ, Packard A. Linear parameter varying control for the X-53 active aeroelastic wing Aiaa Atmospheric Flight Mechanics Conference 2011. |
0.436 |
|
| 2011 |
Seiler P, Vanek B, Bokor J, Balas GJ. Robust H∞ filter design using frequency gridding Proceedings of the American Control Conference. 1801-1806. |
0.619 |
|
| 2010 |
Topcu U, Packard AK, Seiler P, Balas GJ. Robust region-of-attraction estimation Ieee Transactions On Automatic Control. 55: 137-142. DOI: 10.1109/Tac.2009.2033751 |
0.388 |
|
| 2010 |
Topcu U, Packard A, Seiler P, Balas G. Help on SOS [Ask the Experts] Ieee Control Systems Magazine. 30: 18-23. DOI: 10.1109/Mcs.2010.937045 |
0.368 |
|
| 2010 |
Vanek B, Balas GJ, Arndt REA. Linear, parameter-varying control of a supercavitating vehicle Control Engineering Practice. 18: 1003-1012. DOI: 10.1016/J.Conengprac.2010.04.006 |
0.774 |
|
| 2009 |
Bhattacharya R, Balas GJ. Control in computationally constrained environments Ieee Transactions On Control Systems Technology. 17: 589-599. DOI: 10.1109/Tcst.2008.2001919 |
0.649 |
|
| 2009 |
Seiler P, Topcu U, Packard A, Balas G. Parameter-Dependent Lyapunov Functions for Linear Systems With Constant Uncertainties Ieee Transactions On Automatic Control. 54: 2410-2416. DOI: 10.1109/Tac.2009.2029294 |
0.35 |
|
| 2009 |
Balas GJ, Packard AK, Seiler PJ. Uncertain model set calculation from frequency domain data Model-Based Control: Bridging Rigorous Theory and Advanced Technology. 89-105. DOI: 10.1007/978-1-4419-0895-7_6 |
0.323 |
|
| 2009 |
Corno M, Savaresi SM, Balas GJ. On linear-parameter-varying (LPV) slip-controller design for two-wheeled vehicles International Journal of Robust and Nonlinear Control. 19: 1313-1336. DOI: 10.1002/rnc.1381 |
0.491 |
|
| 2009 |
Chakraborty A, Seiler P, Balas GJ. Applications of linear and nonlinear robustness analysis techniques to the F/A-18 flight control laws Aiaa Guidance, Navigation, and Control Conference and Exhibit. |
0.397 |
|
| 2008 |
Wu F, Packard A, Balas G. Systematic Gain-Scheduling Control Design: A Missile Autopilot Example Asian Journal of Control. 4: 341-347. DOI: 10.1111/J.1934-6093.2002.Tb00362.X |
0.478 |
|
| 2008 |
Keviczky T, Borrelli F, Fregene K, Godbole D, Balas GJ. Decentralized receding horizon control and coordination of autonomous vehicle formations Ieee Transactions On Control Systems Technology. 16: 19-33. DOI: 10.1109/Tcst.2007.903066 |
0.698 |
|
| 2008 |
Corno M, Savaresi SM, Balas GJ. Linear, parameter-varying wheel slip control for two-wheeled vehicles Proceedings of the Ieee Conference On Decision and Control. 5030-5035. DOI: 10.1109/CDC.2008.4738924 |
0.501 |
|
| 2008 |
Paw YC, Balas GJ. Parametric uncertainty modeling for LFT model realization Proceedings of the Ieee International Symposium On Computer-Aided Control System Design. 834-839. DOI: 10.1109/CACSD.2008.4627338 |
0.809 |
|
| 2008 |
Paw YC, Balas GJ. Uncertainty modeling, analysis and robust flight control design for a small UAV system Aiaa Guidance, Navigation and Control Conference and Exhibit. |
0.835 |
|
| 2008 |
Hennig A, Balas GJ. MPC supervisory flight controller: A case study to flight EL AL 1862 Aiaa Guidance, Navigation and Control Conference and Exhibit. |
0.434 |
|
| 2007 |
Vanek B, Bokor J, Balas GJ, Arndt REA. Longitudinal motion control of a high-speed supercavitation vehicle Jvc/Journal of Vibration and Control. 13: 159-184. DOI: 10.1177/1077546307070226 |
0.752 |
|
| 2007 |
Keviczky T, Borrelli F, Balas GJ. Distributed Predictive Control: Synthesis, Stability and Feasibility Cooperative Control of Distributed Multi-Agent Systems. 79-108. DOI: 10.1002/9780470724200.ch5 |
0.61 |
|
| 2006 |
Bokor J, Szabó Z, Balas G. Controllability Of Bimodal Lpv Systems Ifac Proceedings Volumes. 39: 89-94. DOI: 10.3182/20060705-3-Fr-2907.00017 |
0.434 |
|
| 2006 |
Ingvalson R, Rotstein HP, Keviczky T, Balas GJ. Fault detection design for uninhabited aerial vehicles Technion Israel Institute of Technology - 46th Israel Annual Conference On Aerospace Sciences 2006. 2: 515-547. DOI: 10.2514/1.16879 |
0.707 |
|
| 2006 |
Rotstein HP, Ingvalson R, Keviczky T, Balas GJ. Fault-detection design for uninhabited aerial vehicles Journal of Guidance, Control, and Dynamics. 29: 1051-1060. DOI: 10.2514/1.16879 |
0.678 |
|
| 2006 |
Keviczky T, Balas GJ. Software-enabled receding horizon control for autonomous unmanned aerial vehicle guidance Journal of Guidance, Control, and Dynamics. 29: 680-694. DOI: 10.2514/1.15562 |
0.737 |
|
| 2006 |
Keviczky T, Balas GJ. Receding horizon control of an F-16 aircraft: A comparative study Control Engineering Practice. 14: 1023-1033. DOI: 10.1016/J.Conengprac.2005.06.003 |
0.711 |
|
| 2006 |
Keviczky T, Borrelli F, Balas GJ. Decentralized receding horizon control for large scale dynamically decoupled systems Automatica. 42: 2105-2115. DOI: 10.1016/j.automatica.2006.07.008 |
0.669 |
|
| 2006 |
Balas GJ, Bokor J, Vanek B, Arndt REA. Control of high-speed underwater vehicles Lecture Notes in Control and Information Sciences. 329: 25-44. DOI: 10.1007/11664550_2 |
0.67 |
|
| 2006 |
Keviczky T, Vanek B, Borrelli F, Balas GJ. Hybrid decentralized receding horizon control of vehicle formations Proceedings of the American Control Conference. 2006: 3358-3363. |
0.79 |
|
| 2006 |
Keviczky T, Fregene K, Borrelli F, Balas GJ, Godbole D. Coordinated autonomous vehicle formations: Decentralization, control synthesis and optimization Proceedings of the American Control Conference. 2006: 2022-2027. |
0.673 |
|
| 2005 |
Marcos A, Mylaraswamy D, Balas GJ. Robust model identification application to a turbofan engine Ifac Proceedings Volumes (Ifac-Papersonline). 16: 880-885. DOI: 10.3182/20050703-6-Cz-1902.00148 |
0.396 |
|
| 2005 |
Bokor J, Balas G. Linear parameter varying systems: A geometric theory and applications Ifac Proceedings Volumes. 38: 12-22. DOI: 10.3182/20050703-6-Cz-1902.00003 |
0.377 |
|
| 2005 |
Szászi I, Marcos A, Balas GJ, Bokor J. Linear parameter-varying detection filter design for a boeing 747-100/200 aircraft Journal of Guidance, Control, and Dynamics. 28: 461-470. DOI: 10.2514/1.6689 |
0.412 |
|
| 2005 |
Arndt REA, Balas GJ, Wosnik M. Control of cavitating flows: A perspective Jsme International Journal, Series B: Fluids and Thermal Engineering. 48: 334-341. DOI: 10.1299/Jsmeb.48.334 |
0.435 |
|
| 2005 |
Keviczky T, Borrelli F, Balas GJ. Stability analysis of decentralized RHC for decoupled systems Proceedings of the 44th Ieee Conference On Decision and Control, and the European Control Conference, Cdc-Ecc '05. 2005: 1689-1694. DOI: 10.1109/CDC.2005.1582402 |
0.658 |
|
| 2005 |
Keviczky T, Packard A, Natale OR, Balas GJ. Application programming interface for real-time receding horizon control Proceedings of the 44th Ieee Conference On Decision and Control, and the European Control Conference, Cdc-Ecc '05. 2005: 1331-1336. DOI: 10.1109/CDC.2005.1582343 |
0.654 |
|
| 2005 |
Marcos A, Balas GJ. Nested integrated control and diagnostic filter design Proceedings of the 44th Ieee Conference On Decision and Control, and the European Control Conference, Cdc-Ecc '05. 2005: 999-1004. DOI: 10.1109/CDC.2005.1582288 |
0.327 |
|
| 2005 |
Marcos A, Ganguli S, Balas GJ. An application of ℋ∞ fault detection and isolation to a transport aircraft Control Engineering Practice. 13: 105-119. DOI: 10.1016/J.Conengprac.2004.02.006 |
0.592 |
|
| 2005 |
Marcos A, Balas GJ. A robust integrated controller/diagnosis aircraft application International Journal of Robust and Nonlinear Control. 15: 531-551. DOI: 10.1002/Rnc.1010 |
0.468 |
|
| 2005 |
Keviczky T, Balas GJ. Software-enabled receding horizon control for autonomous UAV guidance Collection of Technical Papers - Aiaa Guidance, Navigation, and Control Conference. 1: 527-552. |
0.714 |
|
| 2005 |
Keviczky T, Balas GJ. Flight test of a receding horizon controller for autonomous UAV guidance Proceedings of the American Control Conference. 5: 3518-3523. |
0.703 |
|
| 2005 |
Marcos A, Balas GJ, Bokor J. Integrated FDI and control for transport aircraft Collection of Technical Papers - Aiaa Guidance, Navigation, and Control Conference. 2: 889-905. |
0.323 |
|
| 2005 |
Borrelli F, Keviczky T, Balas GJ, Stewart G, Fregene K, Godbole D. Hybrid decentralized control of large scale systems Lecture Notes in Computer Science. 3414: 168-183. |
0.662 |
|
| 2005 |
Belcastro CM, Khong TH, Shin JY, Kwatny H, Chang BC, Balas GJ. Uncertainty modeling for robustness analysis of aircraft control upset prevention and recovery systems Collection of Technical Papers - Aiaa Guidance, Navigation, and Control Conference. 8: 5686-5715. |
0.373 |
|
| 2004 |
Bhattacharya R, Balas GJ. Anytime Control Algorithm: Model Reduction Approach Journal of Guidance Control and Dynamics. 27: 767-776. DOI: 10.2514/1.9457 |
0.554 |
|
| 2004 |
Marcos A, Balas GJ. Development of Linear-Parameter-Varying Models for Aircraft Journal of Guidance, Control, and Dynamics. 27: 218-228. DOI: 10.2514/1.9165 |
0.443 |
|
| 2004 |
Jarvis-Wloszek Z, Philbrick D, Kaya MA, Packard A, Balas G. Control with disturbance preview and online optimization Ieee Transactions On Automatic Control. 49: 266-270. DOI: 10.1109/Tac.2003.822876 |
0.411 |
|
| 2004 |
Borrelli F, Keviczky T, Balas GJ. Collision-free UAV formation flight using decentralized optimization and invariant sets Proceedings of the Ieee Conference On Decision and Control. 1: 1099-1104. DOI: 10.1109/CDC.2004.1428839 |
0.697 |
|
| 2004 |
Keviczky T, Borrelli F, Balas GJ. A study on decentralized receding horizon control for decoupled systems Proceedings of the American Control Conference. 6: 4921-4926. DOI: 10.1109/ACC.2004.249093 |
0.669 |
|
| 2004 |
Balas GJ, Packard AK, Safonov MG, Chiang RY. Next generation of tools for robust control Proceedings of the American Control Conference. 6: 5612-5615. DOI: 10.1109/ACC.2004.249034 |
0.333 |
|
| 2004 |
Bokor J, Balas G. Detection filter design for LPV systems-a geometric approach Automatica. 40: 511-518. DOI: 10.1016/J.Automatica.2003.11.003 |
0.387 |
|
| 2004 |
Keviczky T, Borrelli F, Balas GJ. Hierarchical design of decentralized receding horizon controllers for decoupled systems Proceedings of the Ieee Conference On Decision and Control. 2: 1592-1597. |
0.66 |
|
| 2003 |
Balas GJ. Flight control law design: An industry perspective European Journal of Control. 9: 207-226. DOI: 10.3166/Ejc.9.207-226 |
0.444 |
|
| 2003 |
Balas G, Bokor J, Szabo Z. Invariant subspaces for LPV systems and their applications Ieee Transactions On Automatic Control. 48: 2065-2069. DOI: 10.1109/Tac.2003.819647 |
0.376 |
|
| 2003 |
Marcos A, Ganguli S, Balas GJ. New strategies for fault tolerant control and fault diagnostic Ifac Proceedings Volumes. 36: 269-274. DOI: 10.1016/S1474-6670(17)36504-7 |
0.652 |
|
| 2003 |
Szabó Z, Bokor J, Balas G. Inversion of LPV systems and its application to fault detection Ifac Proceedings Volumes. 36: 233-238. DOI: 10.1016/S1474-6670(17)36499-6 |
0.341 |
|
| 2003 |
Nalbantoğlu V, Bokor J, Balas G, Gaspar P. System identification with generalized orthonormal basis functions: an application to flexible structures Control Engineering Practice. 11: 245-259. DOI: 10.1016/S0967-0661(02)00113-2 |
0.397 |
|
| 2003 |
Bhattacharya R, Balas GJ. An Algorithm for Computationally Efficient Digital Implementation of LTI Controllers Proceedings of the American Control Conference. 2: 1165-1170. |
0.334 |
|
| 2003 |
Keviczky T, Balas GJ. Software enabled flight control using receding horizon techniques Aiaa Guidance, Navigation, and Control Conference and Exhibit. |
0.721 |
|
| 2003 |
Shao Y, Mesbahi M, Balas GJ. Planing, switching, and supercavitating flight control Aiaa Guidance, Navigation, and Control Conference and Exhibit. |
0.362 |
|
| 2002 |
Szabó Z, Bokor J, Balas G. Detection Filter Design For Lpv Systems – A Geometric Approach Ifac Proceedings Volumes. 35: 371-376. DOI: 10.3182/20020721-6-Es-1901.00793 |
0.368 |
|
| 2002 |
Shin JY, Balas GJ, Kaya MA. Blending methodology of linear parameter varying control synthesis of F-16 aircraft system Journal of Guidance, Control, and Dynamics. 25: 1040-1048. DOI: 10.2514/2.5008 |
0.537 |
|
| 2002 |
Bhattacharya R, Balas GJ, Kaya MA, Packard A. Nonlinear Receding Horizon Control of an F-16 Aircraft Journal of Guidance Control and Dynamics. 25: 924-931. DOI: 10.2514/2.4965 |
0.646 |
|
| 2002 |
Fialho I, Balas GJ. Road adaptive active suspension design using linear parameter-varying gain-scheduling Ieee Transactions On Control Systems Technology. 10: 43-54. DOI: 10.1109/87.974337 |
0.492 |
|
| 2002 |
Balas GJ. Linear, parameter-varying control and its application to a turbofan engine International Journal of Robust and Nonlinear Control. 12: 763-796. DOI: 10.1002/Rnc.704 |
0.53 |
|
| 2002 |
Shin JY, Balas GJ. Optimal blending functions in linear parameter varying control synthesis for F-16 aircraft Proceedings of the American Control Conference. 1: 41-46. |
0.363 |
|
| 2002 |
Bhattacharya R, Balas GJ. Implementation of control algorithms in an environment of dynamically scheduled CPU time using balanced truncation Aiaa Guidance, Navigation, and Control Conference and Exhibit. |
0.314 |
|
| 2002 |
Bhattacharya R, Balas GJ, Kaya MA, Packard A. Nonlinear receding horizon control of an F-16 aircraft Journal of Guidance, Control, and Dynamics. 25: 924-931. |
0.387 |
|
| 2001 |
Shin JY, Balas GJ, Packard AK. Worst-case analysis of the X-38 crew return vehicle flight control system Journal of Guidance, Control, and Dynamics. 24: 261-269. DOI: 10.2514/2.4708 |
0.563 |
|
| 2001 |
Bhattacharya R, Balas GJ, Kaya A, Packard A. Nonlinear receding horizon control of F-16 aircraft Proceedings of the American Control Conference. 1: 518-522. |
0.387 |
|
| 2000 |
Barker JM, Balas GJ. Comparing linear parameter-varying gain-scheduled control techniques for active flutter suppression Journal of Guidance, Control, and Dynamics. 23: 948-955. DOI: 10.2514/2.4637 |
0.468 |
|
| 2000 |
Fialho I, Balas GJ, Packard AK, Renfrow J, Mullaney C. Gain-Scheduled Lateral Control of the F-14 Aircraft during Powered Approach Landing Journal of Guidance, Control, and Dynamics. 23: 450-458. DOI: 10.2514/2.4550 |
0.482 |
|
| 2000 |
Lu WW, Balas GJ, Lee EB. Linear quadratic performance with worst case disturbance rejection International Journal of Control. 73: 1516-1524. DOI: 10.1080/00207170050163387 |
0.398 |
|
| 2000 |
Fialho IJ, Balas GJ. Design of nonlinear controllers for active vehicle suspensions using parameter-varying control synthesis Vehicle System Dynamics. 33: 351-370. DOI: 10.1076/0042-3114(200005)33:5;1-Q;Ft351 |
0.53 |
|
| 2000 |
Balas G, Bokor J. Detection Filter Design for LPV Systems Ifac Proceedings Volumes. 33: 641-644. DOI: 10.1016/S1474-6670(17)37432-3 |
0.355 |
|
| 2000 |
Karkoub M, Balas G, Tamma K, Donath M. Robust control of flexible manipulators via μ-synthesis Control Engineering Practice. 8: 725-734. DOI: 10.1016/S0967-0661(00)00006-X |
0.491 |
|
| 2000 |
Mueller JB, Balas GJ. Implementation and testing of LPV controllers for the NASA F/A-18 systems research aircraft Aiaa Guidance, Navigation, and Control Conference and Exhibit. |
0.329 |
|
| 1999 |
Wolodkin G, Balas GJ, Garrard WL. Application of parameter-dependent robust control synthesis to turbofan engines Journal of Guidance, Control, and Dynamics. 22: 833-838. DOI: 10.2514/2.4460 |
0.525 |
|
| 1999 |
Barker JM, Balas GJ, Blue PA. Gain-scheduled linear fractional control for active flutter suppression Journal of Guidance, Control, and Dynamics. 22: 507-512. DOI: 10.2514/2.4418 |
0.465 |
|
| 1999 |
Vipperman JS, Barker JM, Clark RL, Balas GJ. Comparison of μ- and H2-Synthesis Controllers on an Experimental Typical Section Journal of Guidance, Control, and Dynamics. 22: 278-285. DOI: 10.2514/2.4375 |
0.49 |
|
| 1999 |
Karkoub M, Tamma K, Balas G. Robust Control of Two-Link Flexible Manipulators Using the μ-Synthesis Technique Journal of Vibration and Control. 5: 559-576. DOI: 10.1177/107754639900500404 |
0.41 |
|
| 1999 |
Lu WW, Balas GJ, Lee EB. A variational approach to H∞ control with transients Ieee Transactions On Automatic Control. 44: 1875-1879. DOI: 10.1109/9.793727 |
0.448 |
|
| 1999 |
Balas GJ, Young PM. Sensor selection via closed-loop control objectives Ieee Transactions On Control Systems Technology. 7: 692-705. DOI: 10.1109/87.799670 |
0.385 |
|
| 1999 |
Barker JM, Balas GJ. Flight control of a tailless aircraft via linear parameter-varying techniques 1999 Guidance, Navigation, and Control Conference and Exhibit. 941-950. |
0.301 |
|
| 1999 |
Balas GJ, Mueller JB, Barker J. Application of gain-scheduled, multivariable control techniques to the F/A-18 system research aircraft 1999 Guidance, Navigation, and Control Conference and Exhibit. 1-9. |
0.301 |
|
| 1999 |
Ganguli S, Nalbantoglu V, Balas GJ. System identification and design of controllers for the advanced controls technology experimental (ACTEX) flight structure 1999 Guidance, Navigation, and Control Conference and Exhibit. 1-9. |
0.594 |
|
| 1999 |
Shin JY, Balas GJ, Packard AK. Worst case analysis of the flight control system X-38 crew return vehicle 1999 Guidance, Navigation, and Control Conference and Exhibit. 552-562. |
0.391 |
|
| 1999 |
van Etten C, Balas GJ, Bennani S. Linear parametrically varying integrated flight and structural mode control for a flexible aircraft 1999 Guidance, Navigation, and Control Conference and Exhibit. 1342-1352. |
0.378 |
|
| 1998 |
Balas GJ, Packard AK, Renfrow J, Mullaney C, M'Closkey RT. Control of the F-14 aircraft lateral-directional axis during powered approach Journal of Guidance, Control, and Dynamics. 21: 899-908. DOI: 10.2514/2.4323 |
0.472 |
|
| 1998 |
Balas GJ. Synthesis of controllers for the active mass driver system in the presence of uncertainty Earthquake Engineering and Structural Dynamics. 27: 1189-1202. DOI: 10.1002/(Sici)1096-9845(1998110)27:11<1189::Aid-Eqe778>3.0.Co;2-S |
0.458 |
|
| 1998 |
Balas GJ, Ryan J, Shin JY, Garrard WL. A new technique for design of controllers for turbofan engines 34th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit. |
0.433 |
|
| 1997 |
Lim KB, Cox DE, Juang JN, Balas GJ. Validation of an experimentally derived uncertainty model 35th Aerospace Sciences Meeting and Exhibit. 1-12. DOI: 10.2514/2.4262 |
0.481 |
|
| 1997 |
Nalbantoğlu V, Bokor J, Balas G. System Identification with Orthononnal Basis Functions: An Application to Flexible Structures Ifac Proceedings Volumes. 30: 383-388. DOI: 10.1016/S1474-6670(17)42636-X |
0.412 |
|
| 1997 |
Blue PA, Balas GJ. Linear parameter varying control for active flutter suppression 1997 Guidance, Navigation, and Control Conference. 1073-1079. |
0.415 |
|
| 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 |
0.442 |
|
| 1996 |
Reiner J, Balas GJ, Garrard WL. Flight control design using Robust dynamic inversion and time-scale separation Automatica. 32: 1493-1504. DOI: 10.1016/S0005-1098(96)00101-X |
0.542 |
|
| 1996 |
Balas GJ, Lind R, Packard A. Optimally scaled H∞ full information control synthesis with real uncertainty Journal of Guidance, Control, and Dynamics. 19: 854-862. |
0.336 |
|
| 1996 |
Nalbantoğlu V, Balas GJ, Thomson P. The role of performance criteria selection in the control of flexible structures 1996 Guidance, Navigation, and Control Conference and Exhibit. 1-10. |
0.325 |
|
| 1996 |
Balas GJ, Packard A, McCloskey B, Renfrew J, Mullaney C. Design of controllers for the F-14 aircraft lateral-directional axis during powered approach 1996 Guidance, Navigation, and Control Conference and Exhibit. 1-11. |
0.379 |
|
| 1996 |
Lim KB, Balas GJ, Anthony TC. A minimum-norm model validation identification for robust control 1996 Guidance, Navigation, and Control Conference and Exhibit. 1-11. |
0.373 |
|
| 1995 |
Reiner J, Balas GJ, Garrard WL. Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft Journal of Guidance Control and Dynamics. 18: 18-24. DOI: 10.2514/3.56651 |
0.573 |
|
| 1995 |
Balas GJ, Young PM. Control Design for Variations in Structural Natural Frequencies Journal of Guidance Control and Dynamics. 18: 325-332. DOI: 10.2514/3.21387 |
0.433 |
|
| 1995 |
Hougui S, Balas GJ, Garrard WL. Design of a robust dynamic inversion lateral/directional flight controller 1995 Guidance, Navigation, and Control Conference. 738-749. |
0.386 |
|
| 1994 |
Balas GJ, Doyle JC. Control of lightly damped, flexible modes in the controller crossover region Journal of Guidance, Control, and Dynamics. 17: 370-377. DOI: 10.2514/3.21207 |
0.629 |
|
| 1994 |
Balas GJ, Doyle JC. Robustness and Performance Trade-Offs in Control Design for Flexible Structures Ieee Transactions On Control Systems Technology. 2: 352-361. DOI: 10.1109/87.338656 |
0.677 |
|
| 1993 |
Packard A, Doyle J, Balas G. Linear, Multivariable Robust Control With a μ Perspective Journal of Dynamic Systems, Measurement, and Control. 115: 426-438. DOI: 10.1115/1.2899083 |
0.632 |
|
| 1992 |
Packard A, Zhou K, Pandey P, Leonhardson J, Balas G. Optimal, constant I/O similarity scaling for full-information and state-feedback control problems Systems & Control Letters. 19: 271-280. DOI: 10.1016/0167-6911(92)90065-Z |
0.338 |
|
| 1992 |
Lim KB, Balas GJ. Line-of-sight control of the CSI evolutionary model: μ control Proceedings of the American Control Conference. 3: 1996-2000. |
0.374 |
|
| 1990 |
Balas GJ, Doyle JC. Identification of Flexible Structures for Robust Control Ieee Control Systems Magazine. 10: 51-58. DOI: 10.1109/37.56278 |
0.64 |
|
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