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2. 发明公开

EP3102488A1 GESCHLEPPTER AKTIVER FLUGKÖRPER ZUR ERMITTLUNG VON MESSDATEN 有权
标题翻译： GESCHLEPPTER AKTIVERFLUGKÖRPERZUR ERMITTLUNG VON MESSDATEN
公开(公告)号：EP3102488A1
公开(公告)日：2016-12-14
申请号：EP15708707.3
申请日：2015-01-24
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , GERDES, Rüdiger , WATSON, James Bradley
IPC分类号： B64D3/00
CPC分类号： B64D3/00 , B64C9/326 , B64C13/16 , B64C2009/005 , B64D27/24 , B64D45/00 , B64D47/08
摘要： Towed flying objects (01) are towed through the air on a cable by an aircraft and in the process carry out measurements for, for example, environmental observation and monitoring processes in inaccessible areas, for example in the polar regions. The passive navigation by means of the aircraft is hazardous here, in particular at very low heights and when obstacles arise. Known flying objects (01) are controlled independently at the flying height by means of an automatic flight control system and have an adjustment device of the aerofoils which is retracted into the non-deflected home position in the event of malfunctions occurring. The flying object (01) according to the invention is, in contrast, independently fully manoeuvrable in all three spatial directions and has an aileron (21), a pitch elevator (27) and a stabilizer (28). An automatic flight control system (32) has, in addition to a stabilization module (33) which also serves specifically for avoiding dangerous oscillating motions of the flying object (01) when bringing it in, an avoidance module (34) which operates in the three-dimensional space, and a malfunction system (36) which, in the event of a failure of its power supply owing to a malfunction, moves the aileron, pitch elevator and stabilizer (21, 27, 28) into the non-deflected home position in a purely mechanical fashion and securely locks them there, with the result that the flying object (01) can be brought in without manoeuvring operations.
摘要翻译：用于确定测量数据的圆柱形主动式空中平台可锁定到承载电缆，使得机载平台能够通过空气拖动。传感器被配置为确定测量数据和机载平台的飞行位置。布置在机载平台的中部区域的两个翼型件是可调节的，并且连接到被配置为副翼的电气调节装置，以便改变垂直飞行位置。相反的两个第一空气引导表面和两个第二空气引导表面具有分别配置为电梯和方向舵的电调节装置。计算机支持的控制装置包括自动飞行管理系统，其被配置为提供对空中平台的垂直飞行位置的自动控制，并且被配置为控制另外的电气调节装置。

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