RECONFIGURATION CONTROLLING METHOD FOR A ROTORCRAFT HAVING LEFT AND RIGHT SIDE ROTORS, AND RECONFIGURATION CONTROLLING METHOD FOR A TILT ROTOR AIRCRAFT IN THE FIXED-WING MODE
摘要
申请公布号
KR100563931(B1)
申请公布日期
2006.03.17
申请号
KR20050026844
申请日期
2005.03.31
申请人
KOREA AEROSPACE RESEARCH INSTITUTE
发明人
KANG, YOUNG SHIN;AHN, OH SUNG;YOO, CHANG SUN;KIM, JAI MOO;KOO, SAM OK
