| 摘要 |
<P>PROBLEM TO BE SOLVED: To solve a problem that, in a conventional towed body, since posture control is performed following the posture change of a mother aircraft, it is difficult to change the route of the towed body without changing the posture of the mother aircraft, and the instability of the towed body caused by the rapid generation of tension and periodic action of the mother aircraft cannot be compensated. Ž<P>SOLUTION: A flight track intended by a user is inputted by a guiding device before flight or during flight, and the aerial towed body having an acceleration sensor, a gyroscopic sensor, a towed rope tension sensor, drive devices and movable blades is guided and controlled. Thus, the towed body can be made to follow the flight track intended by the user even if tension is rapidly generated, and the posture of the towed body can be controlled stably. Ž<P>COPYRIGHT: (C)2010,JPO&INPIT Ž
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