摘要
控制弹道是控制专业必须的分析工具,也是其他许多专业的开展工作的基础。控制弹道仿真结果的精度与可信性直接影响着地空导弹武器系统的设计、定型结果。控制弹道的程序调试工作是一个较为复杂的过程,需要较强的综合判断能力。对地空导弹武器系统的控制弹道调试过程及仿真结果分析进行了详细论述与说明,并利用飞行试验结果对仿真模型进行了校验。校验结果说明了程序设计的正确性与真实性,同时说明了这种模型校验方法的可行性。
The controlled trajectory is a essential tool for the control accuracy,and also a foundation for other specialism.The accuracy and believability of controlled trajectory simulation results influence design and qualification of surface to air missiles directly.The debugging of controlled trajectory requir more synthetic judgment ability because of its complex.In this paper the debugging process and simulation results are discussed and illustrated in detail,and simulation models are validated and verified via flight experiment data.The validation verification results showed the accuracy and reliability of program design,and feasibility of the model verification.
出处
《火力与指挥控制》
CSCD
北大核心
2010年第6期81-85,共5页
Fire Control & Command Control
关键词
导弹
控制弹道
精度
模型校验
missile
controlled trajectory
accuracy
verification of model
