| 摘要 |
<p>The missile (10) has an optical sensor (11) that is configured for detecting and controlling a target object. A flight propulsion unit configured to influence a trajectory of the missile. A computing unit configured for image processing and flight control of the missile. The optical sensor is formed stationary with respect to the missile. The optical sensor is adapted to form a sensor image with defined number of pixels. A portion of field region of the sensor image is read. The partial region of the sensor image is variable or adjustable. An independent claim is included for a method for tracking a target object of a missile.</p> |
