摘要
运载火箭电测系统靶场测试数据参数类型多、数量大,人工判读测试数据工作量大、效率低,判读准确度难以控制。为了提高靶场电测系统测试判读的效率和准确性,设计了一种基于C/S架构的航天发射场自动判读系统。将参数分为普通参数、台阶参数、脉冲参数、指令参数和复杂曲线参数,针对不同类型的参数,设计不同的算法模型实现智能判读。实际应用表明,该系统能有效提高数据判读比对效率,为航天发射场准确高效决策提供有力支持。
The launch vehicle test data has a huge amount of complex data types.Artificial interpretation of these test data must be a heavy workload,with low efficiency and the interpretation accuracy is difficult to control.In order to improve the efficiency and accuracy of the test data interpretation for electrical measurement systems,an automatic interpretation system based on C/S is designed for launching site.These parameters are divided into common parameters,step parameters,pulse parameters,instruction parameters and complex curve parameters.Different arithmetic models are designed for different types of parameters to realize intelligent interpretation which can effectively improve the efficiency of data interpretation and comparison,and provide a strong support for the accurate and efficient decision-making for launching site.
出处
《兵器装备工程学报》
CAS
2017年第10期122-126,共5页
Journal of Ordnance Equipment Engineering
关键词
运载火箭
电测系统
测试数据
自动判读
航天发射场
launch vehicle
electrical measurement system
test data
automatic interpretation
launching site
