Guided missile control procedure - using on-board camera and transducer data communicating with ground control
摘要
The equipment housed in the nose of the missile includes a video camera. Measurement and picture data are transmitted to the ground station in duplex mode. Control commands are transmitted to the missile. The camera platform is fitted with measurement transducers to give position information in two axes, similar to gyroscope systems. Roll angle is measured and correct by jets. The altitude of the missile is continually monitored. ADVANTAGE - Does not require course correction points to be previously entered in computer to avoid side deviations from flight path.
申请公布号
DE3920643(A1)
申请公布日期
1991.01.10
申请号
DE19893920643
申请日期
1989.06.23
申请人
MESSERSCHMITT-BOELKOW-BLOHM GMBH, 8012 OTTOBRUNN, DE
发明人
HOESSLE, WOLFGANG VON, DIPL.-ING., 8012 RIEMERLING, DE