Integrated guidance and control of moving-mass actuated kinetic warheads PK Menon, GD Sweriduk, EJ Ohlmeyer, DS Malyevac Journal of Guidance, control, and Dynamics 27 (1), 118-126, 2004 | 264 | 2004 |
Integrated Guidance and Control of Missiles With Theta-D Method M Xin, SN Balakrishnan, EJ Ohlmeyer Control Systems Technology, IEEE Transactions on 14 (6), 981-992, 2006 | 256* | 2006 |
Generalized vector explicit guidance EJ Ohlmeyer, CA Phillips Journal of Guidance, Control, and Dynamics 29 (2), 261-268, 2006 | 231 | 2006 |
Integrated design of agile missile guidance and autopilot systems PK Menon, EJ Ohlmeyer Control Engineering Practice 9 (10), 1095-1106, 2001 | 207 | 2001 |
Numerical state-dependent Riccati equation approach for missile integrated guidance control SS Vaddi, PK Menon, EJ Ohlmeyer Journal of guidance, control, and dynamics 32 (2), 699-703, 2009 | 126 | 2009 |
Analysis of an ultra-tightly coupled GPS/INS system in jamming EJ Ohlmeyer Proceedings of IEEE/ION PLANS 2006, 44-53, 2006 | 114 | 2006 |
Nonlinear missile autopilot design with Theta-D technique M Xin, SN Balakrishnan, DT Stansbery, EJ Ohlmeyer Journal of guidance, control, and dynamics 27 (3), 406-417, 2004 | 109 | 2004 |
Root-mean-square miss distance of proportional navigation missile against sinusoidal target EJ Ohlmeyer Journal of Guidance, Control, and Dynamics 19 (3), 563-568, 1996 | 106 | 1996 |
Comparison between nonlinear filtering techniques for spiraling ballistic missile state estimation J Kim, SS Vaddi, PK Menon, EJ Ohlmeyer IEEE Transactions on Aerospace and Electronic Systems 48 (1), 313-328, 2012 | 94 | 2012 |
Optimal design of integrated missile guidance and control CF Lin, J Bibel, E Ohlmeyer, S Malyevac AIAA and SAE, 1998 World Aviation Conference, 5519, 1998 | 68 | 1998 |
Integrated design of agile missile guidance and control systems PK Menon, EJ Ohlmeyer Proceedings of the 7th Mediterranean Conference on Control and Automation 3 …, 1999 | 65 | 1999 |
Nonlinear missile autopilot design using time-scale separation PK Menon, EJ Ohlmeyer | 65 | 1997 |
Nonlinear integrated guidance-control laws for homing missiles E Ohlmeyer, P Menon AIAA Guidance, Navigation, and Control Conference and Exhibit, 4160, 2001 | 59 | 2001 |
Particle filter for ballistic target tracking with glint noise J Kim, M Tandale, PK Menon, E Ohlmeyer Journal of guidance, control, and dynamics 33 (6), 1918-1921, 2010 | 51 | 2010 |
Control of terminal engagement geometry using generalized vector explicit guidance EJ Ohlmeyer Proceedings of the 2003 American Control Conference, 2003. 1, 396-401, 2003 | 41 | 2003 |
Finite-horizon robust integrated guidance-control of a moving-mass actuated kinetic warhead P Menon, S Vaddi, E Ohlmeyer AIAA guidance, navigation, and control conference and exhibit, 6787, 2006 | 40 | 2006 |
Assessment of Integrated GPS/INS for the EX-171 Extended Range Guided Munition EJ Ohlmeyer, TR Pepitone, BL Miller AIAA Guidance, Navigation and Control Conference, 1998 | 39 | 1998 |
Assessment of a GPS guided spinning projectile using an accelerometer-only IMU KB Pamadi, EJ Ohlmeyer AIAA Guidance, Navigation & Control Conference, 2004, 2004 | 38 | 2004 |
Numerical SDRE approach for missile integrated guidance-control S Vaddi, P Menon, E Ohlmeyer AIAA Guidance, Navigation and Control Conference and Exhibit, 6672, 2007 | 35 | 2007 |
GPS-aided navigation system requirements for smart munitions and guided missiles E Ohlmeyer, T Pepitone, B Miller, D Malyevac, J Bibel, A Evans, ... Guidance, Navigation, and Control Conference, 3683, 1997 | 35 | 1997 |