发明名称 Landing method for an unmanned helicopter
摘要 <p>An unmanned helicopter 20 includes altitude control device for giving a command of a collective pitch blade angle based on an altitude change rate command, etc., and performing altitude control of an airframe. The unmanned helicopter further includes descending device for causing the airframe to descend to a second altitude while changing descent rate command of the altitude control device and giving a descent rate command smaller than the descent rate command to the second altitude to the altitude control device for causing the airframe to descend from the second altitude to the ground.</p>
申请公布号 EP2261120(B1) 申请公布日期 2012.06.27
申请号 EP20100181036 申请日期 2003.10.07
申请人 FUJI JUKOGYO KABUSHIKI KAISHA 发明人 YAMANE, AKIHIRO
分类号 G05D1/08;B64C13/20;B64C27/04;B64C39/02;G05D1/06 主分类号 G05D1/08
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