NSSC OpenIR  > 空间技术部
探空火箭有效载荷集成测试软件系统的设计与实现
Alternative TitleDesign and implementation of sounding rocket payloads integrated test software system
陈志敏; 陈萍; 姜秀杰,刘波; Chen, Z.-M. (chenzm@nssc.ac.cn)
Department空间技术部
Source Publication固体火箭技术
2012
Volume35Issue:6Pages:821-825
ISSN1006-2793
Language中文
Abstract为适应国内新一代探空火箭载荷系统的各类测试需求,集成测试软件系统综合采用了组播和USB 等技术;软件算法上实现了相位解模糊、RS译码等功能,解决了载荷数据的校验问题,提高了系统的可靠性。"子午工程"首枚探空火箭成功发射的经验表明,该 软件系统的设计满足探空火箭有效载荷的集成测试需求,具有较好的通用性及可扩展性,有效降低了测试系统的硬件成本。
Other AbstractIn order to meet the various testing requirements of a new generation of sounding rocket payload system, the software system adopts a combination of technologies such as multicasting and USB, and the host computer algorithm has the functions of phase defuzzification and RS decoding. The successful application of the first "Meridian Project" sounding rocket indicated the software system satisfies all the test requirements of sounding rocket payloads. It has good generality and scalability, which reduces the hardware cost.
Indexed ByEI
Document Type期刊论文
Identifierhttp://ir.nssc.ac.cn/handle/122/4760
Collection空间技术部
Corresponding AuthorChen, Z.-M. (chenzm@nssc.ac.cn)
Recommended Citation
GB/T 7714
陈志敏,陈萍,姜秀杰,刘波,等. 探空火箭有效载荷集成测试软件系统的设计与实现[J]. 固体火箭技术,2012,35(6):821-825.
APA 陈志敏,陈萍,姜秀杰,刘波,&Chen, Z.-M. .(2012).探空火箭有效载荷集成测试软件系统的设计与实现.固体火箭技术,35(6),821-825.
MLA 陈志敏,et al."探空火箭有效载荷集成测试软件系统的设计与实现".固体火箭技术 35.6(2012):821-825.
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