| 摘要 |
After a correction or disturbance of the flight attitude, the air-launched body (1) is intended to change quickly back into a smooth flight attitude as a result of a flight stabilisation device at the tail of the air-launched body (1). A plurality of flat elements (4), which can fold, are for this purpose in each case fastened to the circumference of the air-launched body (1) by means of one of their edges (6), which edge extends predominantly in the direction of flight. Each flat element (4) is fastened to a collapsible web (2) by means of its edge (5) which is adjacent to said edge (6). The unfolded collapsible webs (2) hold the flat elements (4) braced in the form of delta wings (7). <IMAGE>
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