摘要
对计及刚体、晃动动力学条件下的运载器系统响应特性进行研究和简化分析，提出精简运动方程的主要思想，推导出动力学响应传递函数零、极点与原始参数之间的数学关系式。最后给出计算结果。
The responding properties of launcher under the conditions of rigid body and shaking dynamics are stadied and analyzed simply. In this paper providing a main thinking for simplifying movement equation,and deriving a mathematic relation between the zero, apex and original parameters in transfer function of dynamical response. Finally the calculating results are given.
出处
《上海航天》
1995年第5期32-36,共5页
Aerospace Shanghai
关键词
运载火箭
控制系统
响应特性
动力学
Launch vehicle, Control system, +￣Responding property,+￣Simplifying calculation
