Jeffrey B. Boka
23Patents
11h-index
17Co-inventors
72Inventor score
Filing activity: Dec 24, 1992 → Jan 15, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7026980B1 | Missile identification and tracking system and method | Physics | 30 | Expired |
| US7511252B1 | Multihypothesis threat missile propagator for boost-phase missile defense | Physics | 27 | Active |
| US5335179A | Unified spacecraft attitude control system with pseudo-complementary paired thrusters | Performing Operations; Transporting | 26 | Expired |
| US8378880B1 | Explicit probabilistic target object selection and engagement | Physics | 23 | Active |
| US9212869B1 | Passive range estimating engagement system and method | Mechanical Engineering; Lighting; Heating | 20 | Active |
| US7473876B1 | Boost phase intercept missile fire control system architecture | Physics | 19 | Active |
| US7411543B1 | Maximum-likelihood rocket identifier | Mechanical Engineering; Lighting; Heating | 16 | Expired |
| US7626534B1 | Unified navigation and inertial target tracking estimation system | Physics | 14 | Active |
| US7181323B1 | Computerized method for generating low-bias estimates of position of a vehicle from sensor data | Physics | 14 | Expired |
| US9250043B1 | System and method for early intercept ballistic missile defense | Performing Operations; Transporting | 12 | Active |
| US8115148B1 | Method for targeting a preferred object within a group of decoys | Mechanical Engineering; Lighting; Heating | 11 | Active |
| US7248206B1 | Instantaneous multisensor angular bias autoregistration | Physics | 11 | Expired |
| US8106340B1 | Generalized midcourse missile guidance | Physics | 9 | Active |
| US7605747B1 | Method for compensating for the positional errors of a sensor | Physics | 9 | Active |
| US7513455B1 | Ballistic missile interceptor guidance by acceleration relative to line-of-sight | Physics | 8 | Expired |
| US8138965B1 | Kinematic algorithm for rocket motor apperception | Physics | 8 | Active |
| US8288696B1 | Inertial boost thrust vector control interceptor guidance | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US8044841B1 | Geometry and sensitivity weighted dynamic multi-sensor selection system and method | Physics | 6 | Active |
| US8134103B2 | Burnout time estimation and early thrust termination determination for a boosting target | Physics | 5 | Active |
| US8130137B1 | Template updated boost algorithm | Physics | 4 | Active |
| US9285190B1 | Correlation/estimation reporting engagement system and method | Physics | 3 | Active |
| US9335127B1 | System and method for defense against radar homing missiles | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10883830B2 | Terrestrial land air and sea navigation system | Physics | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.