| 摘要 |
The present invention relates to an airborne radar (3) notably for a drone (1). The airborne radar (3) has: A first structure (4) is, mechanically attached to an aircraft (1) carrying the radar (3). The first structure (4) has a degree of rotational freedom relative to the aircraft (1) on a first axis (23). A second structure (5) is, attached to the first structure (4). The second structure (5) has a degree of rotational freedom relative to the first structure (4) on a second axis (26) converging with the first axis (23). An antenna (28) receives and sends electromagnetic waves, attached to the second structure (5). An electronic module (40, 41) processes the electromagnetic waves sent or received by the antenna (28). The electronic module (40, 41) is attached to the second structure (5). This invention finds its main application in the field of tactical drones.
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