Methods for stellar-inertial navigation and gyromoment guidance of the agile land-survey satellites
The novel discrete algorithms for signal processing, calibration and alignment of a strapdown inertial navigation system for attitude determination of an agile spacecraft are presented. The problem on synthesis of the attitude guidance laws for an observation spacecraft at land surveying is consider...
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| creator | Somov, Y. Buryrin, S. Somov, S. |
| description | The novel discrete algorithms for signal processing, calibration and alignment of a strapdown inertial navigation system for attitude determination of an agile spacecraft are presented. The problem on synthesis of the attitude guidance laws for an observation spacecraft at land surveying is considered. The spacecraft attitude guidance on selected sequence by interchanging its agile rotation maneuvers with the general boundary conditions and the scanning observation courses is performed by a gyro moment cluster. Numerical results demonstrating efficiency of the developed methods for the stellar-inertial navigation and synthesis of the gyromoment guidance laws at the area land survey are presented. |
| doi_str_mv | 10.1109/RAST.2011.5966975 |
| format | Conference Proceeding |
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The problem on synthesis of the attitude guidance laws for an observation spacecraft at land surveying is considered. The spacecraft attitude guidance on selected sequence by interchanging its agile rotation maneuvers with the general boundary conditions and the scanning observation courses is performed by a gyro moment cluster. Numerical results demonstrating efficiency of the developed methods for the stellar-inertial navigation and synthesis of the gyromoment guidance laws at the area land survey are presented.</description><subject>agile spacecraft</subject><subject>Boundary conditions</subject><subject>Estimation</subject><subject>Extraterrestrial measurements</subject><subject>guidance</subject><subject>land survey</subject><subject>navigation</subject><subject>Position measurement</subject><subject>Quaternions</subject><subject>Silicon compounds</subject><subject>Space vehicles</subject><isbn>9781424496174</isbn><isbn>1424496179</isbn><isbn>9781424496150</isbn><isbn>9781424496167</isbn><isbn>1424496160</isbn><isbn>1424496152</isbn><fulltext>true</fulltext><rsrctype>conference_proceeding</rsrctype><creationdate>2011</creationdate><recordtype>conference_proceeding</recordtype><sourceid>6IE</sourceid><sourceid>RIE</sourceid><recordid>eNpVkM1KAzEUhSMiKHUeQNzkBaYmk0wyd1mKf1ARtPtyZ-ZmGpkfSdLCvL0Vu_FsDgc-vsVh7E6KpZQCHj5Wn9tlIaRclmAM2PKCZWArqQutwchSXP7bVl-zLMYvccoJNxJuWPNGaT-1kbsp8Jio7zHkfqSQPPZ8xKPvMPlp5Di2vJvDNEwDjYl3B9_i2BCfHE974tj5nnh_ovJ4CEeaecRfm08Ub9mVwz5Sdu4F2z49btcv-eb9-XW92uQeRMpdYaCSjaLWoUWoWgeNBQWgrGsc6cqoWikFlZValqbGQghFBLVrai2xUgt2_6f1RLT7Dn7AMO_Oz6gf5-JY8g</recordid><startdate>201106</startdate><enddate>201106</enddate><creator>Somov, Y.</creator><creator>Buryrin, S.</creator><creator>Somov, S.</creator><general>IEEE</general><scope>6IE</scope><scope>6IL</scope><scope>CBEJK</scope><scope>RIE</scope><scope>RIL</scope></search><sort><creationdate>201106</creationdate><title>Methods for stellar-inertial navigation and gyromoment guidance of the agile land-survey satellites</title><author>Somov, Y. ; Buryrin, S. ; Somov, S.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i90t-f26981c3edfa7a98df9c7939937fcfe4863b33398714156ba2003ee9bfcb41a83</frbrgroupid><rsrctype>conference_proceedings</rsrctype><prefilter>conference_proceedings</prefilter><language>eng</language><creationdate>2011</creationdate><topic>agile spacecraft</topic><topic>Boundary conditions</topic><topic>Estimation</topic><topic>Extraterrestrial measurements</topic><topic>guidance</topic><topic>land survey</topic><topic>navigation</topic><topic>Position measurement</topic><topic>Quaternions</topic><topic>Silicon compounds</topic><topic>Space vehicles</topic><toplevel>online_resources</toplevel><creatorcontrib>Somov, Y.</creatorcontrib><creatorcontrib>Buryrin, S.</creatorcontrib><creatorcontrib>Somov, S.</creatorcontrib><collection>IEEE Electronic Library (IEL) Conference Proceedings</collection><collection>IEEE Proceedings Order Plan All Online (POP All Online) 1998-present by volume</collection><collection>IEEE Xplore All Conference Proceedings</collection><collection>IEEE Electronic Library (IEL)</collection><collection>IEEE Proceedings Order Plans (POP All) 1998-Present</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Somov, Y.</au><au>Buryrin, S.</au><au>Somov, S.</au><format>book</format><genre>proceeding</genre><ristype>CONF</ristype><atitle>Methods for stellar-inertial navigation and gyromoment guidance of the agile land-survey satellites</atitle><btitle>Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011</btitle><stitle>RAST</stitle><date>2011-06</date><risdate>2011</risdate><spage>909</spage><epage>914</epage><pages>909-914</pages><isbn>9781424496174</isbn><isbn>1424496179</isbn><eisbn>9781424496150</eisbn><eisbn>9781424496167</eisbn><eisbn>1424496160</eisbn><eisbn>1424496152</eisbn><abstract>The novel discrete algorithms for signal processing, calibration and alignment of a strapdown inertial navigation system for attitude determination of an agile spacecraft are presented. The problem on synthesis of the attitude guidance laws for an observation spacecraft at land surveying is considered. The spacecraft attitude guidance on selected sequence by interchanging its agile rotation maneuvers with the general boundary conditions and the scanning observation courses is performed by a gyro moment cluster. Numerical results demonstrating efficiency of the developed methods for the stellar-inertial navigation and synthesis of the gyromoment guidance laws at the area land survey are presented.</abstract><pub>IEEE</pub><doi>10.1109/RAST.2011.5966975</doi><tpages>6</tpages></addata></record> |
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| language | eng |
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| source | IEEE Electronic Library (IEL) Conference Proceedings |
| subjects | agile spacecraft Boundary conditions Estimation Extraterrestrial measurements guidance land survey navigation Position measurement Quaternions Silicon compounds Space vehicles |
| title | Methods for stellar-inertial navigation and gyromoment guidance of the agile land-survey satellites |
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