摘要
介绍了一种应用Chapman-Kirk方法和分段多项式拟合技术,从弹道测速雷达数据中提取火箭弹的推力和比冲的方法,并给出了详细的数学模型和实际处理结果。
This paper introduces a method for extracting thrust and specific impluse of the rocket from trajectory Doppler Radar Data,using Chapman-Kirk method and polynomial fiting. The detailed mathematical model and processing results are given.
出处
《指挥技术学院学报》
1995年第1期21-25,共5页
Journal of Institute of Command and Technology
关键词
测速雷达
火箭弹
推力
参数辨识
比冲
Trajectory Dopple Radar
Thrust of Rocket
Paameter Identification