| 摘要 |
An aerial video camera (1, 11) has control communication from a universal-control computer (2) and a vibration damper (6, 7, 8). The camera is rotatable circumferentially and tiltable inside of a hemispherical radome (10) that is suspended from a camera pod (9) which is attached to a wing-strut bolt (14) of an aircraft (3) with preferably an attachment bracket (13). Pan and tilt site of the camera are communicated electronically to a monitor (12) of the universal-control computer having a joystick control (20).
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