| 摘要 |
<p>PROBLEM TO BE SOLVED: To accurately detect a position of a flying object and guide a missile to the flying object even if the flying object as a detection target is a flying object greatly low in radar radio wave reflectance and having stealth properties.SOLUTION: A missile guidance system 10 of the present invention includes: position observation means 20 observing a position of a flying object on the basis of a chronological change in a receiving level of a radio wave deriving from outer space, and outputting an observation position (an azimuth angle and an elevation angle from the position observation means 20) of the flying object; a missile 30 outputting a detected position (an azimuth angle and an elevation angle from the missile 30 or the azimuth angle, the elevation angle, and a distance from the missile 30) of the flying object; and guidance means 40 acquiring positional information (an azimuth angle, an elevation angle, and a distance from the guidance means 40) on the missile 30, and guiding the missile 30 in a direction of the flying object on the basis of the acquired positional information on the missile 30 and the output observation position of the flying object.</p> |
