CN102425978A - Missile-borne computer - Google Patents
Missile-borne computer Download PDFInfo
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- CN102425978A CN102425978A CN2011103300998A CN201110330099A CN102425978A CN 102425978 A CN102425978 A CN 102425978A CN 2011103300998 A CN2011103300998 A CN 2011103300998A CN 201110330099 A CN201110330099 A CN 201110330099A CN 102425978 A CN102425978 A CN 102425978A
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Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201110330099.8A CN102425978B (en) | 2011-10-26 | 2011-10-26 | Missile-borne computer |
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CN201110330099.8A CN102425978B (en) | 2011-10-26 | 2011-10-26 | Missile-borne computer |
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CN102425978A true CN102425978A (en) | 2012-04-25 |
CN102425978B CN102425978B (en) | 2014-04-02 |
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CN201110330099.8A Active CN102425978B (en) | 2011-10-26 | 2011-10-26 | Missile-borne computer |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106093629A (en) * | 2016-06-03 | 2016-11-09 | 上海机电工程研究所 | The unit test system of the missile-borne computer of infrared rotary missile and method of testing |
CN109253670A (en) * | 2017-07-13 | 2019-01-22 | 北京信息科技大学 | A kind of more bullet kind fuse flight course parameter measuring apparatus |
CN111366188A (en) * | 2018-12-26 | 2020-07-03 | 北京信息科技大学 | Data acquisition and storage device for dynamic environment force measurement field |
CN111692919A (en) * | 2020-01-16 | 2020-09-22 | 北京理工大学 | Precise guidance control method for aircraft with ultra-close range |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1430720A (en) * | 2000-05-25 | 2003-07-16 | 斯托姆金属有限公司 | Directional control of missiles |
CN101101650A (en) * | 2007-07-02 | 2008-01-09 | 北京理工大学 | Low altitude penetration missile three-dimensional route planning method |
CN201764899U (en) * | 2010-09-19 | 2011-03-16 | 航宇救生装备有限公司 | Multifunctional electric control air starting device |
CN202421893U (en) * | 2011-10-26 | 2012-09-05 | 王伟 | Missile-borne computer |
-
2011
- 2011-10-26 CN CN201110330099.8A patent/CN102425978B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1430720A (en) * | 2000-05-25 | 2003-07-16 | 斯托姆金属有限公司 | Directional control of missiles |
CN101101650A (en) * | 2007-07-02 | 2008-01-09 | 北京理工大学 | Low altitude penetration missile three-dimensional route planning method |
CN201764899U (en) * | 2010-09-19 | 2011-03-16 | 航宇救生装备有限公司 | Multifunctional electric control air starting device |
CN202421893U (en) * | 2011-10-26 | 2012-09-05 | 王伟 | Missile-borne computer |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106093629A (en) * | 2016-06-03 | 2016-11-09 | 上海机电工程研究所 | The unit test system of the missile-borne computer of infrared rotary missile and method of testing |
CN109253670A (en) * | 2017-07-13 | 2019-01-22 | 北京信息科技大学 | A kind of more bullet kind fuse flight course parameter measuring apparatus |
CN109253670B (en) * | 2017-07-13 | 2021-07-30 | 北京信息科技大学 | Multi-bullet detonator flight process parameter measuring device |
CN111366188A (en) * | 2018-12-26 | 2020-07-03 | 北京信息科技大学 | Data acquisition and storage device for dynamic environment force measurement field |
CN111692919A (en) * | 2020-01-16 | 2020-09-22 | 北京理工大学 | Precise guidance control method for aircraft with ultra-close range |
CN111692919B (en) * | 2020-01-16 | 2021-05-28 | 北京理工大学 | Precise guidance control method for aircraft with ultra-close range |
Also Published As
Publication number | Publication date |
---|---|
CN102425978B (en) | 2014-04-02 |
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Legal Events
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
ASS | Succession or assignment of patent right |
Owner name: BEIJING LIGONG UNIVERSITY Free format text: FORMER OWNER: WANG WEI Effective date: 20130710 |
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C41 | Transfer of patent application or patent right or utility model | ||
TA01 | Transfer of patent application right |
Effective date of registration: 20130710 Address after: 100081 No. 5, Zhongguancun South Street, Haidian District, Beijing Applicant after: BEIJING INSTITUTE OF TECHNOLOGY Address before: 100081 No. five South Main Street, Haidian District, Beijing, Zhongguancun Applicant before: Wang Wei |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
EE01 | Entry into force of recordation of patent licensing contract |
Application publication date: 20120425 Assignee: Xi'an Rui Xiang measurement and Control Technology Co., Ltd. Assignor: Beijing Institute of Technology Contract record no.: 2016990000136 Denomination of invention: Missile-borne computer Granted publication date: 20140402 License type: Common License Record date: 20160408 |
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LICC | Enforcement, change and cancellation of record of contracts on the licence for exploitation of a patent or utility model | ||
CB03 | Change of inventor or designer information | ||
CB03 | Change of inventor or designer information |
Inventor after: Lin Defu Inventor after: Wang Wei Inventor after: Wang Jiang Inventor after: Wang Hui Inventor after: Song Tao Inventor after: Cheng Zhenxuan Inventor after: Fan Shipeng Inventor after: Xu Ping Inventor after: Luo Yanwei Inventor before: Wang Wei Inventor before: Lin Defu Inventor before: Wang Jiang Inventor before: Cheng Zhenxuan Inventor before: Xu Ping Inventor before: Wang Hui Inventor before: Song Tao Inventor before: Fan Shipeng Inventor before: Luo Yanwei |