Year |
Citation |
Score |
2020 |
Ram SPA, Akella MR. Uniform Exponential Stability Result for the Rigid-Body Attitude Tracking Control Problem Journal of Guidance Control and Dynamics. 43: 39-45. DOI: 10.2514/1.G004481 |
0.468 |
|
2020 |
Almeida MMd, Mortari D, Zanetti R, Akella M. QuateRA: The Quaternion Regression Algorithm Journal of Guidance Control and Dynamics. 43: 1600-1616. DOI: 10.2514/1.G004375 |
0.313 |
|
2020 |
Vanstone L, Bosco A, Saleh Y, Akella M, Clemens NT, Gogineni S. Closed-Loop Control of Unstart in a Mach 1.8 Isolator Journal of Propulsion and Power. 36: 153-157. DOI: 10.2514/1.B37444 |
0.408 |
|
2020 |
Almeida MMd, Akella MR. New Class of Attitude Controllers Guaranteed to Converge within Specified Finite-Time Journal of the Astronautical Sciences. 67: 552-570. DOI: 10.1007/S40295-019-00180-5 |
0.504 |
|
2019 |
Moghe R, Zanetti R, Akella MR. Adaptive Kalman Filter for Detectable Linear Time-Invariant Systems Journal of Guidance Control and Dynamics. 42: 2197-2205. DOI: 10.2514/1.G004359 |
0.316 |
|
2019 |
Dong H, Hu Q, Liu Y, Akella MR. Adaptive Pose Tracking Control for Spacecraft Proximity Operations Under Motion Constraints Journal of Guidance Control and Dynamics. 42: 2258-2271. DOI: 10.2514/1.G004231 |
0.456 |
|
2019 |
Hu Q, Chi B, Akella MR. Anti-Unwinding Attitude Control of Spacecraft with Forbidden Pointing Constraints Journal of Guidance Control and Dynamics. 42: 822-835. DOI: 10.2514/1.G003606 |
0.38 |
|
2019 |
Hu Q, Chi B, Akella MR. Reduced Attitude Control for Boresight Alignment With Dynamic Pointing Constraints Ieee-Asme Transactions On Mechatronics. 24: 2942-2952. DOI: 10.1109/Tmech.2019.2944431 |
0.554 |
|
2019 |
Dong H, Hu Q, Akella MR, Yang H. Composite Adaptive Attitude-Tracking Control With Parameter Convergence Under Finite Excitation Ieee Transactions On Control Systems and Technology. 1-8. DOI: 10.1109/Tcst.2019.2942802 |
0.434 |
|
2019 |
Dong H, Hu Q, Akella MR, Mazenc F. Partial Lyapunov Strictification: Dual-Quaternion-Based Observer for 6-DOF Tracking Control Ieee Transactions On Control Systems and Technology. 27: 2453-2469. DOI: 10.1109/Tcst.2018.2864723 |
0.534 |
|
2018 |
Vanstone L, Hashemi KE, Lingren J, Akella MR, Clemens NT, Donbar J, Gogineni S. Closed-Loop Control of Shock-Train Location in a Combusting Scramjet Journal of Propulsion and Power. 34: 660-667. DOI: 10.2514/1.B36743 |
0.313 |
|
2018 |
Zhang G, Zhou D, Mortari D, Akella MR. Covariance analysis of Lambert's problem via Lagrange's transfer-time formulation Aerospace Science and Technology. 77: 765-773. DOI: 10.1016/J.Ast.2018.03.039 |
0.392 |
|
2017 |
Dong H, Hu Q, Akella MR. Dual-Quaternion-Based Spacecraft Autonomous Rendezvous and Docking Under Six-Degree-of-Freedom Motion Constraints Journal of Guidance Control and Dynamics. 41: 1150-1162. DOI: 10.2514/1.G003094 |
0.384 |
|
2017 |
Hu Q, Tan X, Akella MR. Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault Journal of Guidance Control and Dynamics. 41: 944-953. DOI: 10.2514/1.G003028 |
0.405 |
|
2017 |
Dong H, Hu Q, Akella MR. Safety Control for Spacecraft Autonomous Rendezvous and Docking Under Motion Constraints Journal of Guidance Control and Dynamics. 1-14. DOI: 10.2514/1.G002322 |
0.403 |
|
2017 |
Hu Q, Tan X, Akella MR. Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation Journal of Guidance Control and Dynamics. 40: 2524-2537. DOI: 10.2514/1.G002191 |
0.46 |
|
2017 |
Yang S, Akella MR, Mazenc F. Dynamically Scaled Immersion and Invariance Adaptive Control for Euler–Lagrange Mechanical Systems Journal of Guidance Control and Dynamics. 40: 2844-2856. DOI: 10.2514/1.G002177 |
0.474 |
|
2017 |
Yang S, Mazenc F, Akella MR. Ultimate Boundedness Results for Noise-Corrupted Quaternion Output Feedback Attitude Tracking Controllers Journal of Guidance Control and Dynamics. 40: 3265-3273. DOI: 10.2514/1.G002164 |
0.423 |
|
2016 |
Yang S, Akella MR, Mazenc F. Immersion and Invariance Observers for Gyro-Free Attitude Control Systems Journal of Guidance Control and Dynamics. 39: 2570-2577. DOI: 10.2514/1.G002095 |
0.456 |
|
2016 |
Hashemi KE, Akella MR, Pak CG. Tracking error convergence for multi-input multi-output model reference adaptive control with known nonminimum phase zeros Proceedings of the Ieee Conference On Decision and Control. 2016: 489-494. DOI: 10.1109/CDC.2015.7402247 |
0.43 |
|
2016 |
Hernandez S, Akella MR. Energy preserving low-thrust guidance for orbit transfers in KS variables Celestial Mechanics and Dynamical Astronomy. 1-26. DOI: 10.1007/S10569-016-9677-0 |
0.367 |
|
2015 |
Hernandez S, Akella MR. Energy-conserving planar spacecraft motion with constant-thrust acceleration Journal of Guidance, Control, and Dynamics. 38: 2309-2323. DOI: 10.2514/1.G000972 |
0.351 |
|
2015 |
Akella MR, Thakur D, Mazenc F. Partial Lyapunov strictification: Smooth angular velocity observers for attitude tracking control Journal of Guidance, Control, and Dynamics. 38: 442-451. DOI: 10.2514/1.G000779 |
0.505 |
|
2015 |
Thakur D, Akella MR. Gyro-Free Rigid-Body Attitude Stabilization Using only Vector Measurements Journal of Guidance Control and Dynamics. 38: 1435-1447. DOI: 10.2514/1.G000623 |
0.345 |
|
2015 |
Thakur D, Srikant S, Akella MR. Adaptive attitude-tracking control of spacecraft with uncertain time-varying inertia parameters Journal of Guidance, Control, and Dynamics. 38: 41-52. DOI: 10.2514/1.G000457 |
0.543 |
|
2015 |
Mazenc F, Yang S, Akella MR. Output feedback, attitude dynamics, robustness 2015 European Control Conference, Ecc 2015. 1249-1254. DOI: 10.1109/ECC.2015.7330711 |
0.457 |
|
2015 |
Mazenc F, Yang S, Akella MR. Time-delayed gyro-free attitude stabilization Proceedings of the American Control Conference. 2015: 3206-3211. DOI: 10.1109/ACC.2015.7171826 |
0.397 |
|
2015 |
Srikant S, Akella M. Arbitrarily fast exponentially stabilizing controller for multi-input, persistently exciting singular control gain systems Automatica. 54: 279-283. DOI: 10.1016/J.Automatica.2015.02.008 |
0.519 |
|
2014 |
Mazenc F, Akella MR. Quaternion-based stabilization of attitude dynamics subject to pointwise delay in the input Proceedings of the American Control Conference. 4877-4882. DOI: 10.2514/1.G001002 |
0.501 |
|
2014 |
Thakur D, Hernandez S, Akella MR. Spacecraft swarm finite-thrust cooperative control for common orbit convergence Advances in the Astronautical Sciences. 152: 2497-2515. DOI: 10.2514/1.G000621 |
0.438 |
|
2014 |
Hutchins KE, Akella MR, Clemens NT, Donbar JM, Gogineni S. Experimental identification of transient dynamics for supersonic inlet unstart Journal of Propulsion and Power. 30: 1605-1612. DOI: 10.2514/1.B35230 |
0.404 |
|
2014 |
Hernandez S, Akella MR. Lyapunov-based guidance for orbit transfers and rendezvous in levi-civita coordinates Journal of Guidance, Control, and Dynamics. 37: 1170-1181. DOI: 10.2514/1.62305 |
0.486 |
|
2014 |
Mercker TH, Akella MR. Adaptive estimation and control algorithms for certain independent control axis misalignments Journal of Guidance, Control, and Dynamics. 37: 72-85. DOI: 10.2514/1.61735 |
0.518 |
|
2014 |
Okamoto M, Akella MR. Avoiding the local-minimum problem in multi-agent systems with limited sensing and communication International Journal of Systems Science. DOI: 10.1080/00207721.2014.965239 |
0.354 |
|
2014 |
Thakur D, Akella MR. Gyro-free rigid body attitude stabilization using only vector measurements on SO(3) Advances in the Astronautical Sciences. 152: 1435-1447. |
0.432 |
|
2014 |
Thakur D, Akella MR. Coordinated control of autonomous vehicles in three-dimensional rotating formations Advances in the Astronautical Sciences. 150: 3137-3147. |
0.36 |
|
2014 |
Hernandez S, Akella MR. A closed-loop solution for spacecraft rendezvous using the KS transformation Advances in the Astronautical Sciences. 150: 507-520. |
0.32 |
|
2013 |
Chunodkar AA, Akella MR. Switching angular velocity observer for rigid-body attitude stabilization and tracking control Advances in the Astronautical Sciences. 148: 223-234. DOI: 10.2514/1.60998 |
0.497 |
|
2013 |
Okamoto M, Akella MR. Novel potential-function-based control scheme for non-holonomic multi-agent systems to prevent the local minimum problem International Journal of Systems Science. 46: 2150-2164. DOI: 10.1080/00207721.2013.858795 |
0.364 |
|
2013 |
Chunodkar AA, Akella MR. Stability of Nonlinear Systems with Unknown Time-varying Feedback Delay Journal of the Astronautical Sciences. 60: 278-302. DOI: 10.1007/S40295-015-0052-2 |
0.462 |
|
2013 |
Hernandez S, Akella MR. Lyapunov-based guidance schemes for in-plane rendezvous using Levi-Civita coordinates Advances in the Astronautical Sciences. 148: 3029-3044. |
0.332 |
|
2013 |
Hernandez S, Akella MR, Ocampo CA. Lyapunov-based elliptical to circular planar orbit transfers in Levi-Civita coordinates Advances in the Astronautical Sciences. 147: 265-279. |
0.324 |
|
2013 |
Chunodkar AA, Akella MR. Switched systems framework for stabilization subject to unknown piece-wise constant feedback delay Advances in the Astronautical Sciences. 147: 137-150. |
0.37 |
|
2012 |
Sukumar S, Akella MR. Persistence filters for estimation: Applications to control in shared-sensing reversible transducer systems Journal of Dynamic Systems, Measurement and Control, Transactions of the Asme. 134. DOI: 10.1115/1.4005510 |
0.482 |
|
2012 |
Valasek J, Akella MR, Siddarth A, Rollins E. Adaptive dynamic inversion control of linear plants with control position constraints Ieee Transactions On Control Systems Technology. 20: 918-933. DOI: 10.1109/Tcst.2011.2159976 |
0.512 |
|
2012 |
Sukumar S, Akella MR. Stabilizing controllers for multi-input, singular control gain systems Proceedings of the Ieee Conference On Decision and Control. 5761-5767. DOI: 10.1109/CDC.2012.6426579 |
0.441 |
|
2012 |
Okamoto M, Akella MR. Adaptive control schemes specially designed for systems with unknown orthogonal matrix parameters Aerospace Science and Technology. 18: 63-68. DOI: 10.1016/J.Ast.2011.04.004 |
0.538 |
|
2012 |
Mercker TH, Akella MR. Adaptive estimation and control algorithms for certain classes of actuator misalignment uncertainties Aiaa Guidance, Navigation, and Control Conference 2012. |
0.485 |
|
2011 |
Mercker TH, Akella MR. Rigid-body attitude tracking with vector measurements and unknown gyro bias Advances in the Astronautical Sciences. 140: 177-196. DOI: 10.2514/1.53111 |
0.523 |
|
2011 |
Chunodkar AA, Akella MR. Attitude stabilization with unknown bounded delay in feedback control implementation Journal of Guidance, Control, and Dynamics. 34: 533-542. DOI: 10.2514/1.50352 |
0.549 |
|
2011 |
Sukumar S, Akella MR. Precision attitude stabilization: Incorporating rise and fall times in gas-based thrusters Journal of Guidance, Control, and Dynamics. 34: 317-323. DOI: 10.2514/1.50068 |
0.472 |
|
2010 |
Chunodkar A, Akella MR. Rigid body attitude stabilization with unknown time-varying delay in feedback Advances in the Astronautical Sciences. 136: 2563-2578. |
0.352 |
|
2010 |
Srikant S, Akella MR. Persistence filter based attitude stabilization of micro-satellites with variable amplitude thrusters Advances in the Astronautical Sciences. 136: 649-659. |
0.375 |
|
2010 |
Summers TH, Chunodkar A, Akella MR. Rigid body attitude synchronization with unknown communication time delays Advances in the Astronautical Sciences. 136: 1155-1164. |
0.334 |
|
2009 |
Summers TH, Akella MR, Mears MJ. Coordinated standoff tracking of moving targets: Control laws and information architectures Journal of Guidance, Control, and Dynamics. 32: 56-69. DOI: 10.2514/1.37212 |
0.432 |
|
2009 |
Srikant S, Akella MR. Persistence filter-based control for systems with time-varying control gains Systems and Control Letters. 58: 413-420. DOI: 10.1016/J.Sysconle.2009.01.010 |
0.494 |
|
2009 |
Seo D, Akella MR. Non-certainty equivalent adaptive control for robot manipulator systems Systems and Control Letters. 58: 304-308. DOI: 10.1016/J.Sysconle.2008.11.008 |
0.495 |
|
2009 |
Chunodkar AA, Akella MR. Attitude stabilization with network delay in feedback control implementation Aiaa Guidance, Navigation, and Control Conference and Exhibit. |
0.402 |
|
2008 |
Seo D, Akella MR. High-performance spacecraft adaptive attitude-tracking control through attracting-manifold design Journal of Guidance, Control, and Dynamics. 31: 884-891. DOI: 10.2514/1.33308 |
0.542 |
|
2008 |
Srikant S, Akella MR. Persistence filters for non-feedback linearizable systems with time-varying control gains Advances in the Astronautical Sciences. 130: 339-345. |
0.411 |
|
2007 |
Seo D, Akella MR. Separation property for the rigid-body attitude tracking control problem Journal of Guidance, Control, and Dynamics. 30: 1569-1576. DOI: 10.2514/1.30296 |
0.566 |
|
2007 |
Summers TH, Akella MR. A non-certainty equivalence approach to decentralized adaptive control 2007 Ieee International Conference On System of Systems Engineering, Sose. DOI: 10.1109/sysose.2007.4304296 |
0.439 |
|
2007 |
Seo D, Akella MR. A separation property for the rigid-body attitude tracking control problem Advances in the Astronautical Sciences. 127: 1199-1212. |
0.463 |
|
2006 |
Akella MR, Seo D, Zanetti R. Attracting manifolds for attitude estimation in flatland and otherlands Journal of the Astronautical Sciences. 54: 635-655. DOI: 10.1007/Bf03256510 |
0.41 |
|
2006 |
Akella MR, Dongeun S, Zanetti R. Attracting manifolds for attitude estimation in flatland and otherlands Journal of the Astronautical Sciences. 54: 635-655. |
0.301 |
|
2005 |
Wallsgrove RJ, Akella MR. Globally stabilizing saturated attitude control in the presence of bounded unknown disturbances Journal of Guidance, Control, and Dynamics. 28: 957-963. DOI: 10.2514/1.9980 |
0.544 |
|
2005 |
Akella MR, Valdivia A, Kotamraju GR. Velocity-free attitude controllers subject to actuator magnitude and rate saturations Journal of Guidance, Control, and Dynamics. 28: 659-666. DOI: 10.2514/1.8784 |
0.517 |
|
2005 |
Subbarao K, Akella MR. Differentiator-free nonlinear proportional-integral controllers for rigid body attitude stabilization Advances in the Astronautical Sciences. 119: 1621-1630. DOI: 10.2514/1.8366 |
0.721 |
|
2005 |
Akella MR. Vision-based adaptive tracking control of uncertain robot manipulators Ieee Transactions On Robotics. 21: 748-753. DOI: 10.1109/Tro.2005.847608 |
0.531 |
|
2005 |
Akella MR, Subbarao K. A novel parameter projection mechanism for smooth and stable adaptive control Systems and Control Letters. 54: 43-51. DOI: 10.1016/J.Sysconle.2004.06.004 |
0.734 |
|
2004 |
Tandale MD, Subbarao K, Valasek J, Akella MR. Structured adaptive model inversion control with actuator saturation constraints applied to tracking spacecraft maneuvers Proceedings of the American Control Conference. 2: 1031-1036. DOI: 10.1109/ACC.2004.182914 |
0.438 |
|
2003 |
Akella MR, Halbert JT, Kotamraju GR. Rigid body attitude control with inclinometer and low-cost gyro measurements Systems and Control Letters. 49: 151-159. DOI: 10.1016/S0167-6911(02)00320-1 |
0.443 |
|
2003 |
Akella MR. Adaptive Control - A Departure from the Certainty-Equivalence Paradigm Advances in the Astronautical Sciences. 115: 370-383. DOI: 10.1007/Bf03546422 |
0.531 |
|
2002 |
Akella MR, Broucke RA. Anatomy of the constant radial thrust problem Journal of Guidance, Control, and Dynamics. 25: 563-570. DOI: 10.2514/2.4917 |
0.328 |
|
2002 |
Ko J, Strganac TW, Junkins JL, Akella MR, Kurdila AJ. Structured model reference adaptive control for a wing section with structural nonlinearity Jvc/Journal of Vibration and Control. 8: 553-573. DOI: 10.1177/107754602023710 |
0.632 |
|
2002 |
Miwa H, Akella MR. Global adaptive stabilization using output feedback for spacecraft attitude tracking Advances in the Astronautical Sciences. 112: 345-357. |
0.67 |
|
2001 |
Kurdila AJ, Strganac TW, Junkins JL, Ko J, Akella MR. Nonlinear control methods for high-energy limit-cycle oscillations Journal of Guidance, Control, and Dynamics. 24: 185-192. DOI: 10.2514/2.4700 |
0.634 |
|
2001 |
Schaub H, Akella MR, Junkins JL. Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics Journal of Guidance, Control, and Dynamics. 24: 95-100. DOI: 10.2514/2.4680 |
0.746 |
|
2001 |
Junkins JL, Akella MR, Kurdila AJ. Adaptive realization of desired constraint stabilization dynamics in the control of multibody systems Philosophical Transactions of the Royal Society a: Mathematical, Physical and Engineering Sciences. 359: 2231-2249. DOI: 10.1098/Rsta.2001.0884 |
0.685 |
|
2001 |
Akella MR. Rigid body attitude tracking without angular velocity feedback Systems and Control Letters. 42: 321-326. DOI: 10.1016/S0167-6911(00)00102-X |
0.47 |
|
2000 |
Akella MR, Alfriend KT. Probability of collision between space objects Journal of Guidance, Control, and Dynamics. 23: 769-772. DOI: 10.2514/2.4611 |
0.312 |
|
2000 |
Akella MR, Kotamraju GR. Trefftz indirect method applied to nonlinear potential problems Engineering Analysis With Boundary Elements. 24: 459-465. DOI: 10.1016/S0955-7997(00)00023-0 |
0.407 |
|
2000 |
Kotamraju GR, Akella MR. Stabilized continuation methods for boundary value problems Applied Mathematics and Computation. 112: 317-332. DOI: 10.1016/S0096-3003(99)00061-2 |
0.486 |
|
2000 |
Schaub H, Akella MR, Junkins JL. Adaptive realization of linear closed-loop tracking dynamics in the presence of large system model errors Journal of the Astronautical Sciences. 48: 537-551. |
0.66 |
|
1999 |
Schaub H, Akella MR, Junkins JL. Adaptive realization of linear closed loop tracking dynamics in the presence of large system model errors Advances in the Astronautical Sciences. 102: 727-743. DOI: 10.1007/Bf03546270 |
0.737 |
|
1999 |
Akella MR, Subbarao K, Junkins JL. Non-linear adaptive auto-pilot for uninhabited aerial combat vehicles 1999 Guidance, Navigation, and Control Conference and Exhibit. 1353-1363. |
0.518 |
|
1998 |
Akella MR, Junkinst JL, Robinett RD. Structured model reference adaptive control with actuator saturation limits Aiaa/Aas Astrodynamics Specialist Conference and Exhibit. 308-315. |
0.317 |
|
1998 |
Akella MR, Junkins JL. Structured model reference adaptive control in the presence of bounded disturbances Advances in the Astronautical Sciences. 99: 375-385. |
0.599 |
|
1997 |
Junkins JL, Akella MR, Robinett RD. Nonlinear adaptive control of spacecraft maneuvers 1997 Guidance, Navigation, and Control Conference. 1-9. DOI: 10.2514/2.4192 |
0.681 |
|
1997 |
Akella MR, Junkins JL. Uncertainty propagation in attitude dynamics Advances in the Astronautical Sciences. 95: 253-268. |
0.603 |
|
1997 |
Akella MR, Junkins JL, Alfriend KT. Some consequences of force model uncertainty on probability of collision with orbital debris Advances in the Astronautical Sciences. 97: 111-121. |
0.534 |
|
1996 |
Junkins JL, Akella MR, Alfriend KT. Non-Gaussian error propagation in orbital mechanics Journal of the Astronautical Sciences. 44: 541-563. |
0.476 |
|
1996 |
Junkins JL, Akella MR, Alfriend KT. Non-Gaussian error propagation in orbital mechanics Journal of the Astronautical Sciences. 44: 541-563. |
0.476 |
|
Show low-probability matches. |