航空学报 > 1993, Vol. 14 Issue (12): 561-566

在非定常气动力作用下弹性飞行器的动稳定性及主动控制

陈士橹, 唐硕, 严恒元, 霍秀芳, 祝小平   

  1. 西北工业大学八系,西安 710072
  • 收稿日期:1992-08-03 修回日期:1993-06-29 出版日期:1993-12-25 发布日期:1993-12-25

DYNAMIC STABILITY AND ACTIVE CONTROL OF ELASTIC VEHICLES WITH UNSTEADY AERODYNAMIC FORCES

Chen Shi-lu, Tang Shuo, Yan Heng-yuan, Huo Xiu-fang, Zhu Xiao-ping   

  1. Eighth Department of Northwestern Polvtechnical University, Xi'an, 710072
  • Received:1992-08-03 Revised:1993-06-29 Online:1993-12-25 Published:1993-12-25

摘要: 首先导出了在非定常气动力作用下的弹性飞行器纵向运动方程。而后就简化的非定常气动力数学模型提出了分析气动弹性对飞行器稳定性影响的方法。并从有效抑制飞行器的弹性振动角度研究主动反馈控制、操纵面及陀螺位置合适选择的最优综合设计问题。

关键词: 非定常气动力, 弹性飞行器, 动稳定性及主动控制

Abstract: In this paper, stability problem of elastic vehicles is studied with the effect of unsteady aerodynamic forces considered. Longitudinal equations of disturbance motions with the actions of unsteady aerodynamic forces are derived. A method of analysis of the effect of aeroelasticity on the stability of elastic vehicles by using a simplified mathematical model of unsteady aerodynamic forces is proposed. Also synthesis of the optimal design of active control system is studied from the view-point of coordinating the design of the active feedback control with the choice of positions of control surfaces and sensors(gyros) locations from the stand point for the efficient suppression of elastic vibrations of the vehicle.

Key words: unsteady aerodynamic forces, elastic vehicles, dynamic stability and active control