节点文献
旋翼-机体耦合动力稳定性的主动控制现状与发展
Active Control Technology of Helicopter Aeromechanic Stability
【摘要】 直升机的地面共振和空中共振主动控制技术是一种新兴的很有发展潜力的技术。目前的控制方法包括桨距控制法和后缘附翼控制法。本文综述国内外学者在这一领域的理论研究工作,并加以评论,指出存在的问题和将来的研究方向。
【Abstract】 Active control of helicopter ‘air and ground resonance’ is a newly developing technology with great potentiality. At present there are two kinds of control approaches: by blade pitch and by trailing edge flap. The theoretical research work in this field is summarized and commented in the paper, such as the mechanism of control, mathematical model, the control law and its design method. The problems and the trends of active control technology for controlling such dynamical stability problem are pointed out, and our points of view are expressed at last.
【关键词】 直升机;
动稳定性;
反馈;
桨距控制;
后缘附翼控制;
【Key words】 helicopters; dynamic stability; feedback; pitch control; flap control;
【Key words】 helicopters; dynamic stability; feedback; pitch control; flap control;
【基金】 航空科学基金
- 【文献出处】 南京航空航天大学学报 ,JOURNAL OF NANJING UNIVERSITY OF AERONAUTICS & ASTRONAUTICS , 编辑部邮箱 ,1997年06期
- 【分类号】V214
- 【被引频次】1
- 【下载频次】95