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Ernest J Ohlmeyer
Ernest J Ohlmeyer
Aero Science Applications LLC, Naval Surface Warfare Center Dahlgren VA
Verified email at kratosdefense.com
Title
Cited by
Cited by
Year
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
2512004
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
243*2006
Generalized vector explicit guidance
EJ Ohlmeyer, CA Phillips
Journal of Guidance, Control, and Dynamics 29 (2), 261-268, 2006
2162006
Integrated design of agile missile guidance and autopilot systems
PK Menon, EJ Ohlmeyer
Control Engineering Practice 9 (10), 1095-1106, 2001
1992001
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
1232009
Analysis of an ultra-tightly coupled GPS/INS system in jamming
EJ Ohlmeyer
Proceedings of IEEE/ION PLANS 2006, 44-53, 2006
1162006
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
1112004
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
1031996
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
922012
Optimal design of integrated missile guidance and control
CF Lin, J Bibel, E Ohlmeyer, S Malyevac
AIAA and SAE, 1998 World Aviation Conference, 5519, 2007
652007
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
651999
Nonlinear missile autopilot design using time-scale separation
PK Menon, EJ Ohlmeyer
621997
Nonlinear integrated guidance-control laws for homing missiles
E Ohlmeyer, P Menon
AIAA Guidance, Navigation, and Control Conference and Exhibit, 4160, 2001
592001
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
472010
Control of terminal engagement geometry using generalized vector explicit guidance
EJ Ohlmeyer
Proceedings of the 2003 American Control Conference, 2003. 1, 396-401, 2003
402003
Assessment of a GPS guided spinning projectile using an accelerometer-only IMU
KB Pamadi, EJ Ohlmeyer
AIAA Guidance, Navigation & Control Conference, 2004, 2004
392004
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
371998
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
362006
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
341997
Numerical SDRE approach for missile integrated guidance-control
S Vaddi, P Menon, E Ohlmeyer
AIAA Guidance, Navigation and Control Conference and Exhibit, 6672, 2007
332007
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