| 摘要 |
Described is a sensor device (10) for a missile (16) having a matrix detector (12) and an electronic evaluation circuit connected thereto. A ray source (20) is stationarily arranged on the missile (16). Provided between the ray source (20) and the matrix detector (12) which is stationarily provided on the missile (16) is a gyro optical device (22) which is cardanically mounted in the missile (16). The sensor device may be employed to determine the roll position and roll rate of a missile (16). |
