摘要
将主动控制技术引入空空导弹总体设计中 ,研究了空空导弹放宽静稳定性设计问题。讨论了放宽静稳定性设计对导弹性能的改善 ,最后给出了静不稳定弹体的系统稳定性判定条件 ,并着重讨论了静不稳定弹体的人工稳定问题。
With introducing the ACT to overall design of an Air to Air Missile(AAM), this thesis analyses the capability improving of the AAM because of using the RRS design, and sets forward the stability criteria for static instability missile body. Finally, it emphatically debates the question of artificial stability for the static instability missile body. The research results have some value to overall design of the AAM.
出处
《飞行力学》
CSCD
2002年第3期55-58,共4页
Flight Dynamics
关键词
主动控制技术
放宽静稳定性
总体设计
空对空导弹
active control technology
relaxed static stability
static instability
artificial stability
