Analytical mechanics of space systems H Schaub, JL Junkins Aiaa, 2003 | 2446 | 2003 |
J2 Invariant Relative Orbits for Spacecraft Formations H Schaub, KT Alfriend Celestial Mechanics and Dynamical Astronomy 79, 77-95, 2001 | 473 | 2001 |
Spacecraft formation flying control using mean orbit elements H Schaub, SR Vadali, JL Junkins, KT Alfriend The Journal of the Astronautical Sciences 48, 69-87, 2000 | 358 | 2000 |
Stereographic orientation parameters for attitude dynamics: A generalization of the Rodrigues parameters H Schaub, JL Junkins Journal of the Astronautical Sciences 44 (1), 1-19, 1996 | 341 | 1996 |
Impulsive feedback control to establish specific mean orbit elements of spacecraft formations H Schaub, KT Alfriend Journal of guidance, control, and dynamics 24 (4), 739-745, 2001 | 240 | 2001 |
Relative orbit geometry through classical orbit element differences H Schaub Journal of Guidance, Control, and Dynamics 27 (5), 839-848, 2004 | 229 | 2004 |
Feedback control law for variable speed control moment gyros H Schaub, SR Vadali, JL Junkins The Journal of the astronautical sciences 46, 307-328, 1998 | 223 | 1998 |
Huber-based divided difference filtering CD Karlgaard, H Schaub Journal of guidance, control, and dynamics 30 (3), 885-891, 2007 | 195 | 2007 |
Challenges and prospects of Coulomb spacecraft formation control H Schaub, GG Parker, LB King The Journal of the Astronautical Sciences 52, 169-193, 2004 | 193* | 2004 |
Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics H Schaub, MR Akella, JL Junkins Journal of Guidance, Control, and Dynamics 24 (1), 95-100, 2001 | 192 | 2001 |
Gravitational perturbations, nonlinearity and circular orbit assumption effects on formation flying control strategies KT Alfriend, DW Gim, H Schaub Guidance and control 2000, 139-158, 2000 | 187 | 2000 |
Singularity avoidance using null motion and variable-speed control moment gyros H Schaub, JL Junkins Journal of Guidance, Control, and Dynamics 23 (1), 11-16, 2000 | 166 | 2000 |
Geosynchronous large debris reorbiter: Challenges and prospects H Schaub, DF Moorer Jr The Journal of the Astronautical Sciences 59 (1), 161-176, 2012 | 142 | 2012 |
Hybrid Cartesian and orbit element feedback law for formation flying spacecraft H Schaub, KT Alfriend Journal of guidance, control, and dynamics 25 (2), 387-393, 2002 | 139 | 2002 |
Linear dynamics and stability analysis of a two-craft Coulomb tether formation A Natarajan, H Schaub Journal of Guidance, Control, and Dynamics 29 (4), 831-839, 2006 | 126 | 2006 |
Analytical charge analysis for two-and three-craft coulomb formations J Berryman, H Schaub Journal of Guidance, Control, and Dynamics 30 (6), 1701-1710, 2007 | 119 | 2007 |
Noncontact position and orientation measurement system and method JL Junkins, D Hughes, H Schaub US Patent 6,266,142, 2001 | 118 | 2001 |
Initial conditions and fuel-optimal control for formation flying of satellites S Vadali, H Schaub, K Alfriend Guidance, Navigation, and Control Conference and Exhibit, 4265, 1999 | 116 | 1999 |
Input shaped large thrust maneuver with a tethered debris object L Jasper, H Schaub Acta Astronautica 96, 128-137, 2014 | 104 | 2014 |
Dynamic and control of spacecraft formations: challenges and some solutions KT Alfriend, H Schaub The Journal of the Astronautical Sciences 48, 249-267, 2000 | 103 | 2000 |