| 摘要 |
<p>The invention has a guidance and control system (44) which includes an optical seeker subsystem (17), a processor subsystem (46), a a three-axis guidance control subsystem (25). The processor subsystem (46) includes a 3-axis MEMs rate sensor (63), a roll algorith device (65), a seeker detection algorithm device (51), and a gudance algorithm device (67). The flight control subsystem (25) includ three canard axis drives (32).</p> |
| 申请人 |
BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.;ZEMANY, PAUL, D.;CARLSON, MARK,A.;MAYNARD, JOHN, A. |
发明人 |
ZEMANY, PAUL, D.;CARLSON, MARK,A.;MAYNARD, JOHN, A. |
