摘要
提出了回收式飞行器系统动态数据的存贮测试方法,研究设计了适用于某飞行器飞行数据测试的存贮测试系统,详细介绍了该系统的系统组成和工作原理,给出了系统的接口设计和信息编码方法,对该系统的抗干扰设计作了详细论述,还给出了该系统的部分实验测试结果。
The article presents the SSFDD(Storage/test System for Flight vehicle's Dynamic Data) methodology in the procedure of an intercontinental missile returning to the ionosphere,and gives the design of the onboard storage/test system for flight data.The article also gives a detailed description about the system construction,the working principle,interface design and the method of information encoding.In addition the pa-per provides a thorough explanation about the system's disturbance-resistant design,and also shows part of the test results of the system.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
1996年第1期36-39,共4页
Acta Armamentarii