Study of Flying Control Computer based on Plug-and-Play Method
被引:0
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作者:
Lin Jin-yong
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机构:
Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R ChinaBeijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R China
Lin Jin-yong
[1
]
Dong Wen-jie
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机构:
Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R ChinaBeijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R China
Dong Wen-jie
[1
]
Wang Yan-ning
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h-index: 0
机构:
Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R ChinaBeijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R China
Wang Yan-ning
[1
]
Liu Jing-jing
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机构:
Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R ChinaBeijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R China
Liu Jing-jing
[1
]
Zhou Chun-mei
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机构:
Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R ChinaBeijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R China
Zhou Chun-mei
[1
]
机构:
[1] Beijing Aerosp Automat Control Inst, Natl Key Lab Sci & Technol Aerosp Intelligence Co, Beijing, Peoples R China
来源:
2014 FOURTH INTERNATIONAL CONFERENCE ON INSTRUMENTATION AND MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC)
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2014年
关键词:
Plug-and-Play;
flying control computer;
aerospace launch vehicle;
design scheme;
D O I:
10.1109/IMCCC.2014.48
中图分类号:
TP [自动化技术、计算机技术];
学科分类号:
0812 ;
摘要:
The applications of plug and play(PnP) method to flying control computer for aerospace launch vehicle is studied, and the plug-and-play model of flying control computer is discussed. Then the PnP design scheme of flying control computer is presented, also the validation experiment is carried through. At last, a simple demonstration system is built, and the research method is tested and analyzed. The test result shows that the above PnP design scheme is correct and will support the future aerospace launch vehicle for upholding the responsive ability.