摘要
根据给定某型号导弹的技术参数 ,综合考虑了各种因素 ,对该导弹飞行过程中弹上接收GPS卫星的情况进行了模拟和分析 ,从而论证了该导弹利用GPS作为外测手段的可行性。
According to the missile's technical parameters and considering every factors , the cases of receiving to GPS signals during the procedure of flying on the missile are simulated and analyzed in this article. The feasibility of using GPS on missile's track measurement is demonstrated.
出处
《宇航计测技术》
CSCD
2001年第2期47-50,共4页
Journal of Astronautic Metrology and Measurement