摘要
反战术弹道导弹的导弹性能很大程度上取决于导弹引信和战斗部,为了提高反战术弹道导弹的毁伤概率,一个简洁而有效的延时估计算法是至关重要的。研究了两种利用导引头角度信息进行的剩余飞行时间估计算法,通过仿真对两种算法进行了分析。根据仿真结果,算法1对导引头角度噪声过于敏感,估计误差太大。算法2相对于算法1具有良好的性能,通过GHK滤波使估计值稳态误差较小,可以满足精确炸点控制要求。
The missile performance of anti-tactical ballistic missile (ATBM) depends on missile fuze and warhead to a great extent. In order to improve the kill probability, a simple but effective time delay algorithm is very important. The paper does some researches on two tlme-to-go algorithms, which are deduced using angle information provided by the seeker fuze and are analyzed through simulation. The simulation results show that the algorithm 1 is too sensitive to the noise of angle and the estimation error is too big. Algorithm 2 has better performance than algorithm 1, GHK filter can make the steady estimation error very small. It can satisfy the request of accurate burst time control.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
2006年第1期27-31,共5页
Acta Armamentarii