Plug-and-play technology-based satellite attitude control ground simulation system
The invention relates to a plug-and-play technology-based satellite attitude control ground simulation system. The simulation system includes an air bearing platform, an embedded attitude control unit, a plug-and-play component, a ground control unit and a display device; the plug-and-play component...
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| creator | LI ZHIJUN CHU JINQIAN HAN DAPENG YUAN FU TU KAIWU SHUI HAITAO ZENG GUOQIANG WU GUOFU LIAN YIJUN XIANG JUNHUA GAO YUDONG LUO TAO |
| description | The invention relates to a plug-and-play technology-based satellite attitude control ground simulation system. The simulation system includes an air bearing platform, an embedded attitude control unit, a plug-and-play component, a ground control unit and a display device; the plug-and-play component is a spaceborne device with an intelligent interface unit; the embedded attitude control unit receives measurement data outputted by a sensor component, and calculates satellite attitude and transmits a control command and outputs the control command to an execution component, and transmits real-time attitude information to the ground control unit; and the ground control unit receives the real-time attitude information transmitted by the embedded attitude control unit and stores the real-time attitude information, and displays the satellite attitude information and the measurement data outputted by the sensor component on the display device in real time, so that the operating process of the simulation system can be observed and monitored. The plug-and-play technology-based satellite attitude control ground simulation system of the invention has high universality. According to the plug-and-play technology-based satellite attitude control ground simulation system adopted, repeated design of the hardware layer of the system is reduced, and the simulation system can be applied to a new application with modification made on software only required, and therefore, a research and development period can be shortened, and cost can be decreased. |
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The simulation system includes an air bearing platform, an embedded attitude control unit, a plug-and-play component, a ground control unit and a display device; the plug-and-play component is a spaceborne device with an intelligent interface unit; the embedded attitude control unit receives measurement data outputted by a sensor component, and calculates satellite attitude and transmits a control command and outputs the control command to an execution component, and transmits real-time attitude information to the ground control unit; and the ground control unit receives the real-time attitude information transmitted by the embedded attitude control unit and stores the real-time attitude information, and displays the satellite attitude information and the measurement data outputted by the sensor component on the display device in real time, so that the operating process of the simulation system can be observed and monitored. The plug-and-play technology-based satellite attitude control ground simulation system of the invention has high universality. According to the plug-and-play technology-based satellite attitude control ground simulation system adopted, repeated design of the hardware layer of the system is reduced, and the simulation system can be applied to a new application with modification made on software only required, and therefore, a research and development period can be shortened, and cost can be decreased.</description><language>eng</language><subject>AIRCRAFT ; AVIATION ; CONTROL OR REGULATING SYSTEMS IN GENERAL ; CONTROLLING ; COSMONAUTICS ; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS ; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</subject><creationdate>2016</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160120&DB=EPODOC&CC=CN&NR=105259794A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160120&DB=EPODOC&CC=CN&NR=105259794A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LI ZHIJUN</creatorcontrib><creatorcontrib>CHU JINQIAN</creatorcontrib><creatorcontrib>HAN DAPENG</creatorcontrib><creatorcontrib>YUAN FU</creatorcontrib><creatorcontrib>TU KAIWU</creatorcontrib><creatorcontrib>SHUI HAITAO</creatorcontrib><creatorcontrib>ZENG GUOQIANG</creatorcontrib><creatorcontrib>WU GUOFU</creatorcontrib><creatorcontrib>LIAN YIJUN</creatorcontrib><creatorcontrib>XIANG JUNHUA</creatorcontrib><creatorcontrib>GAO YUDONG</creatorcontrib><creatorcontrib>LUO TAO</creatorcontrib><title>Plug-and-play technology-based satellite attitude control ground simulation system</title><description>The invention relates to a plug-and-play technology-based satellite attitude control ground simulation system. The simulation system includes an air bearing platform, an embedded attitude control unit, a plug-and-play component, a ground control unit and a display device; the plug-and-play component is a spaceborne device with an intelligent interface unit; the embedded attitude control unit receives measurement data outputted by a sensor component, and calculates satellite attitude and transmits a control command and outputs the control command to an execution component, and transmits real-time attitude information to the ground control unit; and the ground control unit receives the real-time attitude information transmitted by the embedded attitude control unit and stores the real-time attitude information, and displays the satellite attitude information and the measurement data outputted by the sensor component on the display device in real time, so that the operating process of the simulation system can be observed and monitored. The plug-and-play technology-based satellite attitude control ground simulation system of the invention has high universality. According to the plug-and-play technology-based satellite attitude control ground simulation system adopted, repeated design of the hardware layer of the system is reduced, and the simulation system can be applied to a new application with modification made on software only required, and therefore, a research and development period can be shortened, and cost can be decreased.</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>CONTROL OR REGULATING SYSTEMS IN GENERAL</subject><subject>CONTROLLING</subject><subject>COSMONAUTICS</subject><subject>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</subject><subject>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</subject><subject>PERFORMING OPERATIONS</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyjsKAjEQANA0FqLeIR4g4G-RLWVRrETEfhmT2RiYzYTNpMjttfAAVq95c_W4U_EGojOJoGpB-45M7Kt5QUanMwgSBUENIkGKQ205ysSk_cQlfkcYC4EEjjrXLDgu1WwAyrj6uVDry_nZXQ0m7jEnsBhR-u623TS7pj22h9P-n_MBgVI5FQ</recordid><startdate>20160120</startdate><enddate>20160120</enddate><creator>LI ZHIJUN</creator><creator>CHU JINQIAN</creator><creator>HAN DAPENG</creator><creator>YUAN FU</creator><creator>TU KAIWU</creator><creator>SHUI HAITAO</creator><creator>ZENG GUOQIANG</creator><creator>WU GUOFU</creator><creator>LIAN YIJUN</creator><creator>XIANG JUNHUA</creator><creator>GAO YUDONG</creator><creator>LUO TAO</creator><scope>EVB</scope></search><sort><creationdate>20160120</creationdate><title>Plug-and-play technology-based satellite attitude control ground simulation system</title><author>LI ZHIJUN ; CHU JINQIAN ; HAN DAPENG ; YUAN FU ; TU KAIWU ; SHUI HAITAO ; ZENG GUOQIANG ; WU GUOFU ; LIAN YIJUN ; XIANG JUNHUA ; GAO YUDONG ; LUO TAO</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN105259794A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2016</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>CONTROL OR REGULATING SYSTEMS IN GENERAL</topic><topic>CONTROLLING</topic><topic>COSMONAUTICS</topic><topic>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</topic><topic>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><toplevel>online_resources</toplevel><creatorcontrib>LI ZHIJUN</creatorcontrib><creatorcontrib>CHU JINQIAN</creatorcontrib><creatorcontrib>HAN DAPENG</creatorcontrib><creatorcontrib>YUAN FU</creatorcontrib><creatorcontrib>TU KAIWU</creatorcontrib><creatorcontrib>SHUI HAITAO</creatorcontrib><creatorcontrib>ZENG GUOQIANG</creatorcontrib><creatorcontrib>WU GUOFU</creatorcontrib><creatorcontrib>LIAN YIJUN</creatorcontrib><creatorcontrib>XIANG JUNHUA</creatorcontrib><creatorcontrib>GAO YUDONG</creatorcontrib><creatorcontrib>LUO TAO</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LI ZHIJUN</au><au>CHU JINQIAN</au><au>HAN DAPENG</au><au>YUAN FU</au><au>TU KAIWU</au><au>SHUI HAITAO</au><au>ZENG GUOQIANG</au><au>WU GUOFU</au><au>LIAN YIJUN</au><au>XIANG JUNHUA</au><au>GAO YUDONG</au><au>LUO TAO</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Plug-and-play technology-based satellite attitude control ground simulation system</title><date>2016-01-20</date><risdate>2016</risdate><abstract>The invention relates to a plug-and-play technology-based satellite attitude control ground simulation system. The simulation system includes an air bearing platform, an embedded attitude control unit, a plug-and-play component, a ground control unit and a display device; the plug-and-play component is a spaceborne device with an intelligent interface unit; the embedded attitude control unit receives measurement data outputted by a sensor component, and calculates satellite attitude and transmits a control command and outputs the control command to an execution component, and transmits real-time attitude information to the ground control unit; and the ground control unit receives the real-time attitude information transmitted by the embedded attitude control unit and stores the real-time attitude information, and displays the satellite attitude information and the measurement data outputted by the sensor component on the display device in real time, so that the operating process of the simulation system can be observed and monitored. The plug-and-play technology-based satellite attitude control ground simulation system of the invention has high universality. According to the plug-and-play technology-based satellite attitude control ground simulation system adopted, repeated design of the hardware layer of the system is reduced, and the simulation system can be applied to a new application with modification made on software only required, and therefore, a research and development period can be shortened, and cost can be decreased.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
| title | Plug-and-play technology-based satellite attitude control ground simulation system |
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