Year |
Citation |
Score |
2020 |
Kenneally PW, Piggott S, Schaub H. Basilisk: A Flexible, Scalable and Modular Astrodynamics Simulation Framework Journal of Aerospace Information Systems. 17: 496-507. DOI: 10.2514/1.I010762 |
0.313 |
|
2020 |
Maxwell J, Wilson K, Hughes J, Schaub H. Multisphere Method for Flexible Conducting Space Objects: Modeling and Experiments Journal of Spacecraft and Rockets. 57: 225-234. DOI: 10.2514/1.A34560 |
0.366 |
|
2020 |
Hughes JA, Schaub H. Electrostatic Tractor Analysis Using a Measured Flux Model Journal of Spacecraft and Rockets. 57: 207-216. DOI: 10.2514/1.A34359 |
0.437 |
|
2020 |
Trentin JFS, Silva SD, Ribeiro JMDS, Schaub H. Inverted Pendulum Nonlinear Controllers Using Two Reaction Wheels: Design and Implementation Ieee Access. 8: 74922-74932. DOI: 10.1109/Access.2020.2988800 |
0.3 |
|
2020 |
Bengtson MT, Wilson KT, Schaub H. Experimental Results of Electron Method for Remote Spacecraft Charge Sensing Social Work. 18. DOI: 10.1029/2019Sw002341 |
0.334 |
|
2020 |
Maxwell J, Schaub H. Charge-product control approach to electrostatic leader-follower formations in LEO plasma wakes Advances in Space Research. DOI: 10.1016/J.Asr.2020.05.023 |
0.463 |
|
2020 |
Burnett ER, Schaub H. Spacecraft formation and orbit control using differential attitude-dependent solar radiation pressure Advances in Space Research. DOI: 10.1016/J.Asr.2020.03.047 |
0.42 |
|
2020 |
Burnett ER, Schaub H. Study of highly perturbed spacecraft formation dynamics via approximation Advances in Space Research. DOI: 10.1016/J.Asr.2020.02.030 |
0.399 |
|
2020 |
Kenneally PW, Schaub H. Fast spacecraft solar radiation pressure modeling by ray tracing on graphics processing unit Advances in Space Research. 65: 1951-1964. DOI: 10.1016/J.Asr.2019.12.028 |
0.309 |
|
2020 |
Maxwell J, Harris A, Schaub H. Balancing differential drag with Coulomb repulsion in low earth orbit plasma wakes Acta Astronautica. DOI: 10.1016/J.Actaastro.2020.08.021 |
0.524 |
|
2020 |
Teil T, Bateman S, Schaub H. Closed-Loop Software Architecture for Spacecraft Optical Navigation and Control Development Journal of the Astronautical Sciences. 1-25. DOI: 10.1007/S40295-020-00216-1 |
0.315 |
|
2019 |
Aslanov V, Schaub H. Detumbling Attitude Control Analysis Considering an Electrostatic Pusher Configuration Journal of Guidance Control and Dynamics. 42: 900-909. DOI: 10.2514/1.G003966 |
0.39 |
|
2019 |
Hughes JA, Schaub H. Heterogeneous Surface Multisphere Models Using Method of Moments Foundations Journal of Spacecraft and Rockets. 56: 1259-1266. DOI: 10.2514/1.A34434 |
0.423 |
|
2019 |
Hughes J, Schaub H. Rapid Modeling of Electrostatic Forces and Torques Considering Dielectrics Journal of Spacecraft and Rockets. 56: 1680-1688. DOI: 10.2514/1.A34413 |
0.439 |
|
2019 |
Trentin JFS, Silva Sd, Schaub H. Variable Speed Control Moment Gyroscope in an Inverted Pendulum Journal of Dynamic Systems Measurement and Control-Transactions of the Asme. 141. DOI: 10.1115/1.4044273 |
0.329 |
|
2019 |
Maxwell J, Schaub H. Low Earth Orbit Plasma Wake Shaping and Applications to On-Orbit Proximity Operations Ieee Transactions On Plasma Science. 47: 4760-4769. DOI: 10.1109/Tps.2019.2939712 |
0.313 |
|
2019 |
Bengtson M, Hughes J, Schaub H. Prospects and Challenges for Touchless Sensing of Spacecraft Electrostatic Potential Using Electrons Ieee Transactions On Plasma Science. 47: 3673-3681. DOI: 10.1109/Tps.2019.2912057 |
0.353 |
|
2019 |
Wilson K, Schaub H. X-Ray Spectroscopy for Electrostatic Potential and Material Determination of Space Objects Ieee Transactions On Plasma Science. 47: 3858-3866. DOI: 10.1109/Tps.2019.2910576 |
0.309 |
|
2019 |
Hughes J, Schaub H. Spacecraft Electrostatic Force and Torque Expansions Yielding Appropriate Fidelity Measures Journal of the Astronautical Sciences. 66: 46-67. DOI: 10.1007/S40295-019-00154-7 |
0.336 |
|
2019 |
Parsay K, Schaub H. Preliminary Results on Optimal Establishment of Solar Sail Formations Journal of the Astronautical Sciences. 66: 32-45. DOI: 10.1007/S40295-018-00147-Y |
0.351 |
|
2018 |
Allard C, Ramos MD, Schaub H, Kenneally P, Piggott S. Modular Software Architecture for Fully Coupled Spacecraft Simulations Journal of Aerospace Information Systems. 15: 670-683. DOI: 10.2514/1.I010653 |
0.303 |
|
2018 |
Cols-Margenet M, Schaub H, Piggott S. Modular Attitude Guidance: Generating Rotational Reference Motions for Distinct Mission Profiles Journal of Aerospace Information Systems. 15: 335-352. DOI: 10.2514/1.I010554 |
0.362 |
|
2018 |
Harris AT, Petersen CD, Schaub H. Linear Coupled Attitude–Orbit Control Through Aerodynamic Drag Journal of Guidance Control and Dynamics. 43: 122-131. DOI: 10.2514/1.G004521 |
0.362 |
|
2018 |
Ramos MD, Schaub H. Kinematic Steering Law for Conically Constrained Torque-Limited Spacecraft Attitude Control Journal of Guidance Control and Dynamics. 41: 1990-2001. DOI: 10.2514/1.G002873 |
0.417 |
|
2018 |
Allard C, Schaub H, Piggott S. General Hinged Rigid-Body Dynamics Approximating First-Order Spacecraft Solar Panel Flexing Journal of Spacecraft and Rockets. 55: 1291-1299. DOI: 10.2514/1.A34125 |
0.352 |
|
2018 |
Sasaki T, Shimomura T, Schaub H. Robust Attitude Control Using a Double-Gimbal Variable-Speed Control Moment Gyroscope Journal of Spacecraft and Rockets. 55: 1235-1247. DOI: 10.2514/1.A34120 |
0.383 |
|
2018 |
Sasaki T, Alcorn J, Schaub H, Shimomura T. Convex Optimization for Power Tracking of Double-Gimbal Variable-Speed Control Moment Gyroscopes Journal of Spacecraft and Rockets. 55: 541-551. DOI: 10.2514/1.A33944 |
0.415 |
|
2018 |
Bennett T, Schaub H. Contactless electrostatic detumbling of axi-symmetric GEO objects with nominal pushing or pulling Advances in Space Research. 62: 2977-2987. DOI: 10.1016/J.Asr.2018.07.021 |
0.457 |
|
2018 |
Parsay K, Schaub H, Schiff C, Williams T. Improving Magnetosphere In Situ Observations Using Solar Sails Advances in Space Research. 61: 74-88. DOI: 10.1016/J.Asr.2017.07.045 |
0.353 |
|
2018 |
Sasaki T, Shimomura T, Pullen S, Schaub H. Attitude and vibration control with double-gimbal variable-speed control moment gyros Acta Astronautica. 152: 740-751. DOI: 10.1016/J.Actaastro.2018.08.047 |
0.407 |
|
2018 |
Schaub H, Piggott S. Speed-constrained three-axes attitude control using kinematic steering Acta Astronautica. 147: 1-8. DOI: 10.1016/J.Actaastro.2018.03.022 |
0.43 |
|
2018 |
Peters TV, Valero JFB, Olmos DE, Lappas V, Jakowski P, Gray I, Tsourdos A, Schaub H, Biesbroek R. Attitude control analysis of tethered de-orbiting Acta Astronautica. 146: 316-331. DOI: 10.1016/J.Actaastro.2018.03.016 |
0.436 |
|
2018 |
Fulton J, Schaub H. Fixed-axis electric sail deployment dynamics analysis using hub-mounted momentum control Acta Astronautica. 144: 160-170. DOI: 10.1016/J.Actaastro.2017.11.048 |
0.4 |
|
2018 |
Ingram G, Hughes J, Bennett T, Reilly C, Schaub H. Volume Multi-Sphere-Model Development Using Electric Field Matching Journal of the Astronautical Sciences. 65: 377-399. DOI: 10.1007/S40295-018-0136-X |
0.399 |
|
2018 |
Panicucci P, Allard C, Schaub H. Spacecraft Dynamics Employing a General Multi-tank and Multi-thruster Mass Depletion Formulation Journal of the Astronautical Sciences. 65: 423-447. DOI: 10.1007/S40295-018-0133-0 |
0.462 |
|
2018 |
Hughes J, Schaub H. Rapid Charged Geosynchronous Debris Perturbation Modeling of Electrodynamic Disturbances Journal of the Astronautical Sciences. 65: 135-156. DOI: 10.1007/S40295-017-0127-3 |
0.465 |
|
2018 |
Hughes J, Schaub H. Space Weather Influence on Electromagnetic Geosynchronous Debris Perturbations Using Statistical Fluxes Social Work. 16: 391-405. DOI: 10.1002/2017Sw001768 |
0.45 |
|
2017 |
Lubey DP, Schaub H. Instantaneous Quadratic Power-Optimal Attitude Tracking with N Control Moment Gyroscopes Journal of Guidance Control and Dynamics. 40: 702-709. DOI: 10.2514/1.G001659 |
0.311 |
|
2017 |
Hughes J, Schaub H. Prospects of Using a Pulsed Electrostatic Tractor With Nominal Geosynchronous Conditions Ieee Transactions On Plasma Science. 45: 1887-1897. DOI: 10.1109/Tps.2017.2684621 |
0.385 |
|
2017 |
Parsay K, Schaub H. Drift-free solar sail formations in elliptical Sun-synchronous orbits Acta Astronautica. 139: 201-212. DOI: 10.1016/J.Actaastro.2017.06.027 |
0.434 |
|
2017 |
Anderson PV, Schaub H. Geosynchronous Debris Conjunction Lead-Time Requirements for Autonomous Low-Thrust Disposal Guidance Journal of the Astronautical Sciences. 64: 188-206. DOI: 10.1007/S40295-016-0106-0 |
0.339 |
|
2016 |
Bennett T, Schaub H. Continuous-Time Modeling and Control Using Nonsingular Linearized Relative-Orbit Elements Journal of Guidance Control and Dynamics. 39: 2605-2614. DOI: 10.2514/1.G000366 |
0.474 |
|
2016 |
Anderson PV, McKnight DS, Di Pentino F, Schaub H. Merging analytic and empirical GEO debris synchronization dynamics Advances in Space Research. 58: 914-923. DOI: 10.1016/J.Asr.2016.05.034 |
0.372 |
|
2016 |
Anderson PV, Schaub H. Conjunction challenges of low-thrust geosynchronous debris removal maneuvers Acta Astronautica. 123: 154-164. DOI: 10.1016/J.Actaastro.2016.03.014 |
0.342 |
|
2016 |
Baresi N, Scheeres DJ, Schaub H. Bounded relative orbits about asteroids for formation flying and applications Acta Astronautica. 123: 364-375. DOI: 10.1016/J.Actaastro.2015.12.033 |
0.424 |
|
2016 |
Stevenson D, Schaub H. Electrostatic spacecraft rate and attitude control - Experimental results and performance considerations Acta Astronautica. 119: 22-33. DOI: 10.1016/J.Actaastro.2015.10.023 |
0.422 |
|
2016 |
McManus L, Schaub H. Establishing a Formation of Small Satellites in a Lunar Flower Constellation Journal of the Astronautical Sciences. 63: 263-286. DOI: 10.1007/S40295-016-0096-Y |
0.33 |
|
2016 |
Hogan EA, Schaub H. Space Weather Influence on Relative Motion Control using the Touchless Electrostatic Tractor Journal of the Astronautical Sciences. 63: 237-262. DOI: 10.1007/S40295-016-0090-4 |
0.767 |
|
2016 |
Allard C, Schaub H, Piggott S. General hinged solar panel dynamics approximating first-order spacecraft flexing Advances in the Astronautical Sciences. 157: 1043-1054. |
0.317 |
|
2015 |
Roscoe CWT, Westphal JJ, Griesbach JD, Schaub H. Formation establishment and reconfiguration using differential elements in J2-perturbed orbits Journal of Guidance, Control, and Dynamics. 38: 1725-1740. DOI: 10.2514/1.G000999 |
0.354 |
|
2015 |
Hogan EA, Schaub H. Three-axis attitude control using redundant reaction wheels with continuous momentum dumping Journal of Guidance, Control, and Dynamics. 38: 1865-1871. DOI: 10.2514/1.G000812 |
0.749 |
|
2015 |
Hogan EA, Schaub H. General High-Altitude Orbit Corrections Using Electrostatic Tugging with Charge Control Journal of Guidance Control and Dynamics. 38: 699-705. DOI: 10.2514/1.G000092 |
0.786 |
|
2015 |
Hogan EA, Schaub H. Impacts of Hot Space Plasma and Ion Beam Emission on Electrostatic Tractor Performance Ieee Transactions On Plasma Science. 43: 3115-3129. DOI: 10.1109/Tps.2015.2451001 |
0.727 |
|
2015 |
Bennett T, Stevenson D, Hogan E, Schaub H. Prospects and challenges of touchless electrostatic detumbling of small bodies Advances in Space Research. 56: 557-568. DOI: 10.1016/J.Asr.2015.03.037 |
0.778 |
|
2015 |
Hogan EA, Schaub H. Impacts of tug and debris sizes on electrostatic tractor charging performance Advances in Space Research. 55: 630-638. DOI: 10.1016/J.Asr.2014.10.023 |
0.752 |
|
2015 |
Bennett T, Schaub H, Roscoe CWT. Faster-than-natural spacecraft circumnavigation via way points Acta Astronautica. DOI: 10.1016/J.Actaastro.2016.01.025 |
0.428 |
|
2015 |
Parsay K, Schaub H. Designing solar sail formations in sun-synchronous orbits for geomagnetic tail exploration Acta Astronautica. 107: 218-233. DOI: 10.1016/J.Actaastro.2014.11.018 |
0.408 |
|
2015 |
Bennett T, Schaub H. Touchless electrostatic Three-dimensional detumbling of large Axi-symmetric debris Journal of the Astronautical Sciences. 62: 233-253. DOI: 10.1007/S40295-015-0075-8 |
0.484 |
|
2015 |
Saaj CM, Lappas V, Richie D, Schaub H. Hybrid propulsion using electrostatic forces for spacecraft swarms 2007 European Control Conference, Ecc 2007. 3187-3194. |
0.374 |
|
2014 |
O'Keefe SA, Schaub H. Shadow set considerations for modified rodrigues parameter attitude filtering Journal of Guidance, Control, and Dynamics. 37: 2030-2034. DOI: 10.2514/1.G000405 |
0.306 |
|
2014 |
Anderson PV, Schaub H. N-impulse formation flying feedback control using nonsingular element description Journal of Guidance, Control, and Dynamics. 37: 540-548. DOI: 10.2514/1.60766 |
0.377 |
|
2014 |
Hogan EA, Schaub H. Attitude parameter inspired relative motion descriptions for relative orbital motion control Journal of Guidance, Control, and Dynamics. 37: 741-749. DOI: 10.2514/1.60626 |
0.757 |
|
2014 |
Jones DR, Schaub H. Collinear three-craft coulomb formation stability analysis and control Journal of Guidance, Control, and Dynamics. 37: 224-232. DOI: 10.2514/1.60293 |
0.502 |
|
2014 |
Inampudi R, Schaub H. Orbit radial dynamic analysis of two-craft Coulomb formation at libration points Journal of Guidance, Control, and Dynamics. 37: 682-691. DOI: 10.2514/1.55282 |
0.831 |
|
2014 |
Seubert CR, Stiles LA, Schaub H. Effective Coulomb force modeling for spacecraft in Earth orbit plasmas Advances in Space Research. 54: 209-220. DOI: 10.1016/J.Asr.2014.04.005 |
0.794 |
|
2014 |
Schaub H, Sternovsky Z. Active space debris charging for contactless electrostatic disposal maneuvers Advances in Space Research. 53: 110-118. DOI: 10.1016/J.Asr.2013.10.003 |
0.406 |
|
2014 |
Jasper L, Schaub H. Tethered towing using open-loop input-shaping and discrete thrust levels Acta Astronautica. 105: 373-384. DOI: 10.1016/J.Actaastro.2014.10.001 |
0.767 |
|
2014 |
Anderson PV, Schaub H. Longitude-dependent effects of fragmentation events in the geosynchronous orbit regime Advances in the Astronautical Sciences. 152: 1699-1715. DOI: 10.1016/J.Actaastro.2014.09.011 |
0.342 |
|
2014 |
Jasper L, Schaub H. Input shaped large thrust maneuver with a tethered debris object Acta Astronautica. 96: 128-137. DOI: 10.1016/J.Actaastro.2013.11.005 |
0.765 |
|
2014 |
Anderson PV, Schaub H. Local debris congestion in the geosynchronous environment with population augmentation Acta Astronautica. 94: 619-628. DOI: 10.1016/J.Actaastro.2013.08.023 |
0.305 |
|
2014 |
O'Keefe SA, Schaub H. Sun-direction estimation using a partially underdetermined set of coarse sun sensors Journal of the Astronautical Sciences. 61: 85-106. DOI: 10.1007/S40295-015-0058-9 |
0.326 |
|
2014 |
Bennett T, Schaub H. Touchless electrostatic three-dimensional detumbling of large GEO debris Advances in the Astronautical Sciences. 152: 2465-2478. |
0.413 |
|
2014 |
Jasper L, Schaub H. Discretized input shaping for a large thrust tethered debris object Advances in the Astronautical Sciences. 152: 3385-3403. |
0.324 |
|
2013 |
Nazari M, Butcher EA, Schaub H. Spacecraft attitude stabilization using nonlinear delayed multiactuator control and inverse dynamics Journal of Guidance, Control, and Dynamics. 36: 1440-1452. DOI: 10.2514/1.58249 |
0.408 |
|
2013 |
Schaub H, Jasper LEZ. Orbit boosting maneuvers for two-craft coulomb formations Journal of Guidance, Control, and Dynamics. 36: 74-82. DOI: 10.2514/1.57479 |
0.503 |
|
2013 |
Hogan EA, Schaub H. Relative motion control for two-spacecraft electrostatic orbit corrections Journal of Guidance, Control, and Dynamics. 36: 240-249. DOI: 10.2514/1.56118 |
0.806 |
|
2013 |
Stevenson D, Schaub H. Optimization of sphere population for electrostatic multi-sphere method Ieee Transactions On Plasma Science. 41: 3526-3535. DOI: 10.1109/Tps.2013.2283716 |
0.396 |
|
2013 |
Anderson PV, Schaub H. Local orbital debris flux study in the geostationary ring Advances in Space Research. 51: 2195-2206. DOI: 10.1016/J.Asr.2013.01.019 |
0.318 |
|
2013 |
Stevenson D, Schaub H. Multi-Sphere Method for modeling spacecraft electrostatic forces and torques Advances in Space Research. 51: 10-20. DOI: 10.1016/J.Asr.2012.08.014 |
0.515 |
|
2013 |
Jones DR, Schaub H. Periodic relative orbits of two spacecraft subject to differential gravity and electrostatic forcing Acta Astronautica. 89: 21-30. DOI: 10.1016/J.Actaastro.2013.03.028 |
0.49 |
|
2013 |
Jasch PD, Hogan EA, Schaub H. Out-of-plane stability analysis of collinear spinning three-craft Coulomb formations Acta Astronautica. 88: 89-97. DOI: 10.1016/J.Actaastro.2013.03.005 |
0.779 |
|
2013 |
Stiles LA, Schaub H, Maute KK, Moorer DF. Electrostatically inflated gossamer space structure voltage requirements due to orbital perturbations Acta Astronautica. 84: 109-121. DOI: 10.1016/J.Actaastro.2012.11.007 |
0.359 |
|
2013 |
Jones DR, Schaub H. Optimal reconfigurations of two-craft Coulomb formations along manifolds Acta Astronautica. 83: 108-118. DOI: 10.1016/J.Actaastro.2012.10.028 |
0.47 |
|
2013 |
Schaub H, Stevenson D. Prospects of relative attitude control using coulomb actuation Advances in the Astronautical Sciences. 147: 119-135. DOI: 10.1007/S40295-015-0048-Y |
0.514 |
|
2012 |
Hogan EA, Schaub H. Attitude parameter inspired descriptions of relative orbital motion Aiaa/Aas Astrodynamics Specialist Conference 2012. DOI: 10.2514/6.2012-4739 |
0.744 |
|
2012 |
Panosian S, Seubert CR, Schaub H. Tethered coulomb structure applied to close proximity situational awareness Journal of Spacecraft and Rockets. 49: 1183-1193. DOI: 10.2514/1.A32212 |
0.798 |
|
2012 |
Inampudi R, Schaub H. Optimal reconfigurations of two-craft coulomb formation in circular orbits Journal of Guidance, Control, and Dynamics. 35: 1805-1815. DOI: 10.2514/1.56551 |
0.806 |
|
2012 |
Stevenson D, Schaub H. Nonlinear control analysis of a double-gimbal variable-speed control moment gyroscope Journal of Guidance, Control, and Dynamics. 35: 787-793. DOI: 10.2514/1.56104 |
0.417 |
|
2012 |
Wang S, Schaub H. One-dimensional constrained coulomb structure control with charge saturations Ieee Transactions On Aerospace and Electronic Systems. 48: 3-15. DOI: 10.1109/Taes.2012.6129617 |
0.699 |
|
2012 |
Hogan EA, Schaub H. Collinear invariant shapes for three-spacecraft Coulomb formations Acta Astronautica. 72: 78-89. DOI: 10.1016/J.Actaastro.2011.10.020 |
0.76 |
|
2012 |
Schaub H, Moorer DF. Geosynchronous large debris reorbiter: Challenges and prospects Journal of the Astronautical Sciences. 59: 165-180. DOI: 10.1007/S40295-013-0011-8 |
0.493 |
|
2012 |
Inampudi R, Schaub H. Disturbance compensating control of orbit radially aligned two-craft Coulomb formation Celestial Mechanics and Dynamical Astronomy. 112: 445-458. DOI: 10.1007/S10569-012-9403-5 |
0.815 |
|
2012 |
Hogan EA, Schaub H. Linear stability and shape analysis of spinning three-craft Coulomb formations Celestial Mechanics and Dynamical Astronomy. 112: 131-148. DOI: 10.1007/S10569-011-9387-6 |
0.783 |
|
2012 |
Stevenson D, Schaub H. Multi Sphere Modeling for electrostatic forces on three-dimensional spacecraft shapes Advances in the Astronautical Sciences. 143: 91-106. |
0.377 |
|
2012 |
Stevenson D, Schaub H. Nonlinear control analysis of a Double-Gimbal Variable-speed control moment gyro Advances in the Astronautical Sciences. 142: 2581-2594. |
0.311 |
|
2012 |
Schaub H, Jasper LEZ. Circular orbit radius control using electrostatic actuation for 2-craft configurations Advances in the Astronautical Sciences. 142: 1479-1495. |
0.454 |
|
2012 |
Jasper LEZ, Schaub H. Effective sphere modeling for electrostatic forces on three-dimensional spacecraft shapes Advances in the Astronautical Sciences. 142: 947-965. |
0.37 |
|
2012 |
Hogan EA, Schaub H. Space debris reorbiting using electrostatic actuation Advances in the Astronautical Sciences. 144: 73-92. |
0.759 |
|
2012 |
Seubert CR, Panosian S, Schaub H. Analysis of a tethered coulomb structure applied to close proximity situational awareness Advances in the Astronautical Sciences. 142: 3527-3546. |
0.79 |
|
2012 |
Stiles LA, Seubert CR, Schaub H. Effective Coulomb force modeling in a space environment Advances in the Astronautical Sciences. 143: 71-89. |
0.785 |
|
2012 |
Jasch PD, Hogan EA, Schaub H. Stability analysis and out-of-plane control of collinear spinning three-craft Coulomb formations Advances in the Astronautical Sciences. 143: 747-762. |
0.766 |
|
2012 |
Jasper LEZ, Seubert CR, Schaub H, Trushkyakov V, Yutkin E. Tethered tug for large low Earth orbit debris removal Advances in the Astronautical Sciences. 143: 2223-2242. |
0.782 |
|
2011 |
Seubert CR, Panosian S, Schaub H. Attitude and power analysis of two-node multitethered coulomb structures Journal of Spacecraft and Rockets. 48: 1033-1045. DOI: 10.2514/1.52185 |
0.777 |
|
2011 |
Wang S, Schaub H. Nonlinear charge control for a collinear fixed-shape three-craft equilibrium Journal of Guidance, Control, and Dynamics. 34: 359-366. DOI: 10.2514/1.52117 |
0.668 |
|
2011 |
Seubert CR, Schaub H. Rotational stiffness study of two-element tethered coulomb structures Journal of Spacecraft and Rockets. 48: 488-497. DOI: 10.2514/1.49772 |
0.799 |
|
2011 |
Wang S, Schaub H. Coulomb control of nonequilibrium fixed shape triangular three-vehicle cluster Journal of Guidance, Control, and Dynamics. 34: 259-270. DOI: 10.2514/1.47835 |
0.66 |
|
2011 |
Wang S, Schaub H. Nonlinear feedback control of a spinning two-spacecraft coulomb virtual structure Ieee Transactions On Aerospace and Electronic Systems. 47: 2055-2067. DOI: 10.1109/Taes.2011.5937282 |
0.685 |
|
2011 |
Inampudi R, Schaub H. Two-craft tether formation relative equilibria about circular orbits and libration points Acta Astronautica. 68: 1761-1773. DOI: 10.1016/J.Actaastro.2011.02.003 |
0.786 |
|
2010 |
Seubert CR, Schaub H. Closed-loop charged relative motion experiments simulating constrained orbital motion Journal of Guidance, Control, and Dynamics. 33: 1856-1865. DOI: 10.2514/1.48274 |
0.828 |
|
2010 |
Mullen J, Schaub H. Hypersphere stereographic orientation parameters Advances in the Astronautical Sciences. 136: 1903-1914. DOI: 10.2514/1.46783 |
0.306 |
|
2010 |
McMahon J, Schaub H. Simplified singularity avoidance using Variable Speed Control Moment Gyroscope null motion Advances in the Astronautical Sciences. 136: 1611-1623. DOI: 10.2514/1.45433 |
0.424 |
|
2010 |
Wang S, Schaub H. Electrostatic spacecraft collision avoidance using piecewise-constant charges Journal of Guidance, Control, and Dynamics. 33: 510-520. DOI: 10.2514/1.44397 |
0.647 |
|
2010 |
Schaub H, Hussein II. Stability and reconfiguration analysis of a circularly spinning two-craft Coulomb tether Ieee Transactions On Aerospace and Electronic Systems. 46: 1675-1686. DOI: 10.1109/Taes.2010.5595587 |
0.519 |
|
2010 |
Saaj CM, Lappas V, Schaub H, Izzo D. Hybrid propulsion system for formation flying using electrostatic forces Aerospace Science and Technology. 14: 348-355. DOI: 10.1016/J.Ast.2010.02.009 |
0.472 |
|
2010 |
Wang S, Schaub H. Switched Lyapunov function based Coulomb control of a triangular 3-vehicle cluster Advances in the Astronautical Sciences. 135: 1477-1496. |
0.346 |
|
2010 |
Wang S, Schaub H. Nonlinear Coulomb feedback control of a spinning two spacecraft virtual structure Advances in the Astronautical Sciences. 135: 1517-1532. |
0.432 |
|
2010 |
Inampudi R, Schaub H. Two-craft Coulomb formation relative equilibria about circular orbits and Libration points Advances in the Astronautical Sciences. 136: 961-980. |
0.311 |
|
2010 |
Seubert CR, Schaub H. Closed-loop one-dimensional charged relative motion experiments simulating constrained orbital motion Advances in the Astronautical Sciences. 135: 1459-1476. |
0.815 |
|
2010 |
Seubert CR, Schaub H. Impact of nodal attitude motion on two-element tethered Coulomb structures Advances in the Astronautical Sciences. 136: 2495-2514. |
0.799 |
|
2010 |
Seubert CR, Schaub H. Electrostatic force model for terrestrial experiments on the coulomb testbed 61st International Astronautical Congress 2010, Iac 2010. 1: 557-565. |
0.796 |
|
2009 |
Schaub H, Lappas VJ. Redundant reaction wheel torque distribution yielding instantaneous L 2 power-optimal attitude control Journal of Guidance, Control, and Dynamics. 32: 1269-1276. DOI: 10.2514/1.41070 |
0.32 |
|
2009 |
Natarajan A, Schaub H. Hybrid control of orbit normal and along-track two-craft Coulomb tethers Aerospace Science and Technology. 13: 183-191. DOI: 10.1016/J.Ast.2008.10.002 |
0.52 |
|
2009 |
Hussein I, Schaub H. Stability and control of relative equilibria for the three-spacecraft Coulomb tether problem Acta Astronautica. 65: 738-754. DOI: 10.1016/j.actaastro.2009.03.035 |
0.372 |
|
2009 |
Seubert CR, Schaub H. Tethered coulomb structures: Prospects and challenges Journal of the Astronautical Sciences. 57: 347-368. DOI: 10.1007/Bf03321508 |
0.808 |
|
2009 |
Wang S, Schaub H. Electrostatic spacecraft collision avoidance using piece-wise constant charges Advances in the Astronautical Sciences. 134: 1251-1270. |
0.343 |
|
2009 |
Seubert CR, Schaub H. One-dimensional testbed for Coulomb controlled spacecraft Advances in the Astronautical Sciences. 134: 205-221. |
0.817 |
|
2008 |
Wang S, Schaub H. Spacecraft collision avoidance using coulomb forces with separation distance and rate feedback Journal of Guidance, Control, and Dynamics. 31: 740-750. DOI: 10.2514/1.29634 |
0.68 |
|
2008 |
Schaub H. Rate-based ship-mounted crane payload pendulation control system Control Engineering Practice. 16: 132-145. DOI: 10.1016/J.Conengprac.2007.04.011 |
0.424 |
|
2008 |
Hussein II, Schaub H. Stability and control of relative equilibria for the three-spacecraft coulomb tether problem Advances in the Astronautical Sciences. 129: 295-313. DOI: 10.1016/J.Actaastro.2009.03.035 |
0.473 |
|
2008 |
Vasavada H, Schaub H. Analytic solutions for equal mass four-craft static Coulomb formation Journal of the Astronautical Sciences. 56: 17-40. DOI: 10.1007/Bf03256540 |
0.437 |
|
2008 |
Vasavada H, Schaub H. Analytic solutions for equal mass 4-craft static coulomb formation Advances in the Astronautical Sciences. 129: 275-294. |
0.325 |
|
2008 |
Wang S, Schaub H. 1-D Constrained coulomb structure stabilization with charge saturation Advances in the Astronautical Sciences. 129: 257-274. |
0.431 |
|
2007 |
Doebbler J, Spaeths T, Valasek J, Monda MJ, Schaub H. Boom and receptacle autonomous air refueling using visual snake optical sensor Journal of Guidance, Control, and Dynamics. 30: 1753-1769. DOI: 10.2514/1.28305 |
0.306 |
|
2007 |
Berryman J, Schaub H. Analytical charge analysis for two- and three-craft coulomb formations Journal of Guidance, Control, and Dynamics. 30: 1701-1710. DOI: 10.2514/1.23785 |
0.458 |
|
2007 |
Schaub H, Hussein I. Stability and reconfiguration analysis of a circularly spinning 2-craft coulomb tether Ieee Aerospace Conference Proceedings. DOI: 10.1109/AERO.2007.352670 |
0.435 |
|
2007 |
Southward CM, Ellis JR, Schaub H. Symmetrie stereographic orientation parameters applied to constrained spacecraft attitude control Journal of the Astronautical Sciences. 55: 389-405. DOI: 10.1007/Bf03256531 |
0.395 |
|
2007 |
Wang S, Schaub H. Spacecraft collision avoidance using Coulomb forces with separation distance feedback Advances in the Astronautical Sciences. 127: 197-216. |
0.409 |
|
2007 |
Natarajan A, Schaub H. Hybrid control of orbit normal and along-track 2-craft Coulomb tethers Advances in the Astronautical Sciences. 127: 1373-1392. |
0.425 |
|
2007 |
Southward CM, Ellis JR, Schaub H. Spacecraft attitude control using Symmetric Stereographic Orientation Parameters Advances in the Astronautical Sciences. 127: 1225-1242. |
0.33 |
|
2007 |
Lappas V, Saaj C, Richie D, Peck M, Streetman B, Schaub H. Spacecraft formation flying and reconfiguration with electrostatic forces Advances in the Astronautical Sciences. 127: 217-225. |
0.362 |
|
2007 |
Saaj CM, Lappas V, Richie D, Schaub H, Izzo D. Hybrid propulsion system for spacecraft swarm aggregation using coulomb force Jbis - Journal of the British Interplanetary Society. 60: 268-274. |
0.362 |
|
2007 |
Natarajan A, Schaub H, Parker GG. Reconfiguration of a nadir-pointing 2-craft Coulomb tether Jbis - Journal of the British Interplanetary Society. 60: 209-218. |
0.358 |
|
2006 |
Natarajan A, Schaub H. Linear dynamics and stability analysis of a two-craft coulomb tether formation Journal of Guidance, Control, and Dynamics. 29: 831-838. DOI: 10.2514/1.16480 |
0.527 |
|
2006 |
Kim M, Schaub H. Coulomb formation conservation laws using differential orbit elements Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 220: 463-474. DOI: 10.1243/09544100JAERO39 |
0.456 |
|
2006 |
Hussein II, Schaub H. Invariant shape solutions of the spinning three craft coulomb tether problem Advances in the Astronautical Sciences. 124: 2015-2033. DOI: 10.1007/S10569-006-9043-8 |
0.394 |
|
2006 |
Schaub H, Hall CD, Berryman J. Necessary conditions for circularly-restricted static coulomb formations Journal of the Astronautical Sciences. 54: 525-541. DOI: 10.1007/Bf03256504 |
0.468 |
|
2006 |
Natarajan A, Schaub H, Parker GG. Reconfiguration of a 2-craft coulomb tether Advances in the Astronautical Sciences. 124: 2035-2050. |
0.355 |
|
2006 |
Berryman J, Schaub H. Analytical charge analysis for 2- and 3-craft Coulomb formations Advances in the Astronautical Sciences. 123: 445-460. |
0.379 |
|
2006 |
Schaub H, Hall CD, Berryman J. Necessary conditions for circularly-restricted static coulomb formations Journal of the Astronautical Sciences. 54: 525-541. |
0.364 |
|
2005 |
Schaub H. Stabilization of satellite motion relative to a Coulomb spacecraft formation Journal of Guidance, Control, and Dynamics. 28: 1231-1239. DOI: 10.2514/1.8577 |
0.518 |
|
2005 |
Natarajan A, Schaub H. Linear dynamics and stability analysis of a coulomb tether formation Advances in the Astronautical Sciences. 120: 1635-1649. |
0.426 |
|
2005 |
Berryman J, Schaub H. Static equilibrium configurations in geo Coulomb spacecraft formations Advances in the Astronautical Sciences. 120: 51-68. |
0.372 |
|
2004 |
Schaub H. Relative orbit geometry through classical orbit element differences Journal of Guidance, Control, and Dynamics. 27: 839-848. DOI: 10.2514/1.12595 |
0.441 |
|
2004 |
Schaub H, Parker GG, King LB. Challenges and prospects of Coulomb spacecraft formation control Journal of the Astronautical Sciences. 52: 169-193. DOI: 10.1007/Bf03546427 |
0.364 |
|
2004 |
Schaub H, Kim M. Differential orbit element constraints for Coulomb satellite formations Collection of Technical Papers - Aiaa/Aas Astrodynamics Specialist Conference. 2: 1035-1048. |
0.467 |
|
2003 |
Agostini MJ, Parker GG, Schaub H, Groom K, Robinett RD. Generating swing-suppressed maneuvers for crane systems with rate saturation Ieee Transactions On Control Systems Technology. 11: 471-481. DOI: 10.1109/Tcst.2003.813402 |
0.391 |
|
2003 |
Schaub H. Incorporating secular drifts into the orbit element difference description of relative orbits Advances in the Astronautical Sciences. 114: 239-257. |
0.311 |
|
2003 |
Schaub H, Parker GG, King LB. Challenges and prospects of coulomb spacecraft formations Advances in the Astronautical Sciences. 115: 351-370. |
0.432 |
|
2001 |
Schaub H, Alfriend KT. Impulsive feedback control to establish specific mean orbit elements of spacecraft formations Journal of Guidance, Control, and Dynamics. 24: 739-745. DOI: 10.2514/2.4774 |
0.459 |
|
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 |
0.735 |
|
2001 |
Alfriend KT, Vadali SR, Schaub H. Formation flying satellites: Control by an astrodynamicist Celestial Mechanics and Dynamical Astronomy. 81: 57-62. DOI: 10.1023/A:1013307103630 |
0.396 |
|
2001 |
Schaub H, Alfriend KT. J2 invariant relative orbits for spacecraft formations Celestial Mechanics and Dynamical Astronomy. 79: 77-95. DOI: 10.1023/A:1011161811472 |
0.378 |
|
2000 |
Schaub H, Alfriend KT. Hybrid Cartesian and orbit element feedback law for formation flying spacecraft Astrodynamics Specialist Conference. 184-191. DOI: 10.2514/2.4893 |
0.437 |
|
2000 |
Schaub H, Junkins JL. Singularity avoidance using null motion and variable-speed control moment gyros Journal of Guidance, Control, and Dynamics. 23: 11-16. DOI: 10.2514/2.4514 |
0.628 |
|
2000 |
Alfriend KT, Schaub H. Dynamic and control of spacecraft formations: Challenges and some solutions Journal of the Astronautical Sciences. 48: 249-267. DOI: 10.1007/Bf03546279 |
0.446 |
|
2000 |
Schaub H, Vadali SR, Junkins JL, Alfriend KT. Spacecraft formation flying control using mean orbit elements Advances in the Astronautical Sciences. 103: 163-181. DOI: 10.1007/Bf03546219 |
0.597 |
|
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 |
0.718 |
|
1998 |
Schaub H, Vadali SR, Junkins JL. Feedback control law for variable speed control moment gyros Journal of the Astronautical Sciences. 46: 307-328. DOI: 10.1007/Bf03546239 |
0.623 |
|
1997 |
Robinett RD, Parker GG, Schaub H, Junkins JL. Lyapunov optimal saturated control for nonlinear systems 35th Aerospace Sciences Meeting and Exhibit. DOI: 10.2514/2.4189 |
0.61 |
|
1997 |
Junkins JL, Schaub H. Orthogonal square root eigenfactor parameterization of mass matrices Journal of Guidance, Control, and Dynamics. 20: 1118-1124. DOI: 10.2514/2.4166 |
0.512 |
|
1997 |
Schaub H, Junkins JL, Robinett RD. New penalty functions and optimal control formulation for spacecraft attitude control problems Journal of Guidance, Control, and Dynamics. 20: 428-434. DOI: 10.2514/2.4093 |
0.545 |
|
1997 |
Tsiotras P, Junkins JL, Schaub H. Higher-order Cayley transforms with applications to attitude representations Journal of Guidance, Control, and Dynamics. 20: 528-534. DOI: 10.2514/2.4072 |
0.511 |
|
1997 |
Junkins JL, Schaub H. An instantaneous eigenstructure quasivelocity formulation for nonlinear multibody dynamics Journal of the Astronautical Sciences. 45: 279-295. DOI: 10.1007/Bf03546405 |
0.551 |
|
1995 |
Schaub H, Tsiotras P, Junkins JL. Principal rotation representations of proper N × N orthogonal matrices International Journal of Engineering Science. 33: 2277-2295. DOI: 10.1016/0020-7225(95)00070-E |
0.504 |
|
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