位置：成果数据库 > 期刊 > 期刊详情页
Stability of Spinning Missiles with an Acceleration Autopilot
  • ISSN号：0731-5090
  • 期刊名称：Journal of Guidance, Control, and Dynamics
  • 时间：0
  • 页码：774-786
  • 相关项目：自旋类弹箭飞行器锥形运动稳定性问题研究
作者： Li, Keyong|Yang, Shuxing|Zhao, Liangyu|
同期刊论文项目
自旋类弹箭飞行器锥形运动稳定性问题研究
期刊论文 10 会议论文 2
同项目期刊论文
提高卷弧翼火箭弹圆锥运动渐近稳定性的几个方法
Coning Motion of Spinning Missiles Induced by the Rate Loop
Analysis on Stability of Coning Motion of Rockets Based on Nutation Theory
Weighted stochastic response surface method considering sample weights
A Nonlinear Optimal Guidance Law with Terminal Impact Angle Constraint
Stability Limits of Spinning Missiles with Attitude Autopilot
A double weighted stochastic response surface method for reliability analysis
Uncertainty quantification for a flapping airfoil with a stochastic velocity deviation
Analysis on Stability of Coning Motion of Rockets Based on Nutation Theory