[{"data":1,"prerenderedAt":302},["ShallowReactive",2],{"navbar-links":3,"contact-information":67,"footer":105,"newsletter":166,"equipment-custom-page-gnc-platform":185},{"data":4,"meta":66},{"id":5,"createdAt":6,"updatedAt":7,"publishedAt":8,"documentId":9,"cta":10,"links":16},19,"2024-02-08T07:06:55.275Z","2026-05-21T09:05:07.595Z","2026-05-21T09:05:08.644Z","b9lt6fvy8dtxc8oec9p9xg8k",{"id":11,"text":12,"buttonStyle":13,"link":14,"square":15,"opacity":15,"bigFullWidth":15},238,"Contact Us","primary","\u002Fcontact",null,[17,22,26,30,34,62],{"id":18,"label":19,"link":20,"__component":21},215,"SATELLITE MODULES","\u002Fmodules","information.link",{"id":23,"label":24,"link":25,"__component":21},216,"SATELLITE PLATFORMS","\u002Fsatellites",{"id":27,"label":28,"link":29,"__component":21},217,"TURNKEY SOLUTIONS","\u002Fturnkey-solutions",{"id":31,"label":32,"link":33,"__component":21},218,"MISSION SERVICES","\u002Fmission-services",{"id":5,"label":35,"links":36,"__component":61},"COMPANY",[37,41,45,49,53,57],{"id":38,"label":39,"link":40},220,"About","\u002Fabout",{"id":42,"label":43,"link":44},221,"History","\u002Fhistory",{"id":46,"label":47,"link":48},222,"Team","\u002Fteam",{"id":50,"label":51,"link":52},223,"Current Job Openings","\u002Fcareer",{"id":54,"label":55,"link":56},224,"Heritage","\u002Fheritage",{"id":58,"label":59,"link":60},225,"Quality & Process","\u002Fquality-process","information.link-group",{"id":63,"label":64,"link":65,"__component":21},219,"NEWS","\u002Fnews",{},{"data":68,"meta":104},{"id":69,"phone":70,"email":71,"copyright":72,"createdAt":73,"updatedAt":74,"publishedAt":75,"documentId":76,"address":77,"socialMedia":85},6,"+45 31 20 82 10","info@space-inventor.com","© 2015 - 2026 Space Inventor A\u002FS All Rights Reserved","2024-02-07T11:42:47.383Z","2026-02-16T09:30:09.641Z","2026-02-16T09:30:09.756Z","p4smt8pc8ty3b4tkbpp5y2mv",{"id":78,"name":79,"address":80,"city":81,"zipcode":82,"country":83,"cvr":84},11,"Space Inventor A\u002FS","Selma Lagerløfs Vej 312 ","Aalborg","9220","Denmark","VAT: DK37053252",[86],{"id":87,"link":88,"logo":89},5,"https:\u002F\u002Fwww.linkedin.com\u002Fcompany\u002Fspace-inventor",{"id":90,"name":91,"alternativeText":92,"caption":15,"width":93,"height":94,"formats":15,"hash":95,"ext":96,"mime":97,"size":98,"url":99,"previewUrl":15,"provider":100,"provider_metadata":15,"createdAt":101,"updatedAt":101,"documentId":102,"publishedAt":103,"focalPoint":15},378,"🦆 icon _linkedin_.png","linkedin",40,39,"icon_linkedin_317dad2c8e",".png","image\u002Fpng",0.28,"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Ficon_linkedin_317dad2c8e.png","strapi-provider-upload-strapi-cloud","2024-04-10T08:41:00.981Z","i3e9cj85xx3fjr6iqv9n44ze","2025-02-03T11:07:39.898Z",{},{"data":106,"meta":165},{"id":107,"documentId":108,"motto":109,"createdAt":110,"updatedAt":110,"publishedAt":111,"logo":112,"links":147},2,"h40nqgl8by3l19iyiph2brfs","\u003Cp>Make Space for Progress\u003C\u002Fp>","2026-05-28T12:29:27.208Z","2026-05-28T12:29:27.760Z",{"id":113,"name":114,"alternativeText":15,"caption":15,"width":115,"height":116,"formats":117,"hash":142,"ext":96,"mime":97,"size":143,"url":144,"previewUrl":15,"provider":100,"provider_metadata":15,"createdAt":145,"updatedAt":145,"documentId":146,"publishedAt":145,"focalPoint":15},663,"si-foot.png",640,250,{"small":118,"xsmall":126,"thumbnail":134},{"ext":96,"url":119,"hash":120,"mime":97,"name":121,"path":15,"size":122,"width":123,"height":124,"sizeInBytes":125},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fsmall_si_foot_2b7fdcd80f.png","small_si_foot_2b7fdcd80f","small_si-foot.png",44.82,500,195,44818,{"ext":96,"url":127,"hash":128,"mime":97,"name":129,"path":15,"size":130,"width":131,"height":132,"sizeInBytes":133},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fxsmall_si_foot_2b7fdcd80f.png","xsmall_si_foot_2b7fdcd80f","xsmall_si-foot.png",21.44,300,117,21440,{"ext":96,"url":135,"hash":136,"mime":97,"name":137,"path":15,"size":138,"width":139,"height":140,"sizeInBytes":141},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fthumbnail_si_foot_2b7fdcd80f.png","thumbnail_si_foot_2b7fdcd80f","thumbnail_si-foot.png",16.16,245,96,16163,"si_foot_2b7fdcd80f",13.49,"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fsi_foot_2b7fdcd80f.png","2026-05-20T08:55:20.420Z","utn0f8olytwgkb3y3g981rgb",[148,151,154,157,161],{"id":149,"label":150,"link":25},231,"Satellites",{"id":152,"label":153,"link":20},232,"Modules",{"id":155,"label":156,"link":44},233,"Achievements",{"id":158,"label":159,"link":160},234,"Privacy Policy","\u002Fprivacy-policy",{"id":162,"label":163,"link":164},235,"Resource Library","\u002Fresource-library",{},{"data":167,"meta":184},{"id":87,"title":168,"agreementText":169,"createdAt":170,"updatedAt":171,"publishedAt":172,"documentId":173,"image":174},"Subscribe to our space corner, where you’ll be updated on everything we have to offer","I understand that Space Inventor can store and analyze data entered in this form along with my browsing activities in order to fulfill my request and\u002For provide an improved user experience. ","2024-02-22T12:57:36.888Z","2026-02-11T08:39:41.306Z","2026-02-11T08:39:41.356Z","do144i1ghmis8d4hkedcee7e",{"id":175,"name":176,"alternativeText":15,"caption":15,"width":15,"height":15,"formats":15,"hash":177,"ext":178,"mime":179,"size":180,"url":181,"previewUrl":15,"provider":100,"provider_metadata":15,"createdAt":182,"updatedAt":182,"documentId":183,"publishedAt":103,"focalPoint":15},376,"VID Footer.mp4","VID_Footer_9c4b760d2a",".mp4","video\u002Fmp4",1384.5,"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002FVID_Footer_9c4b760d2a.mp4","2024-04-09T06:15:00.373Z","r043e1eh5ue96h937nhpul7s",{},{"data":186,"meta":298},[187],{"id":188,"documentId":189,"slug":190,"createdAt":191,"updatedAt":192,"publishedAt":193,"seo":194,"components":201},28,"mzwdyvasswtdvlg67nts6xg2","gnc-platform","2026-02-05T15:30:39.478Z","2026-02-06T11:42:41.635Z","2026-02-06T11:42:41.786Z",{"id":195,"metaTitle":196,"metaDescription":197,"keywords":198,"metaRobots":199,"structuredData":15,"metaViewport":15,"canonicalURL":15,"metaImage":15,"metaSocial":200},157,"Space Inventor - Modular Power Platform","Space Inventor creates revolutionary satellites and satellite modules","satellite,space,aerospace,satellite components,satellite modules,satellite parts","all",[],[202,206,266,273,276,280,290,294],{"id":203,"content":204,"__component":205},335,"\u003Ch1>Guidance, Navigation, and Control (GNC) Platform&nbsp;\u003C\u002Fh1>\u003Cp class=\"p1\">Complete, Scalable Guidance, Navigation &amp; Control System for CubeSats and MicroSats.\u003Cbr>\u003Cbr>Space Inventor’s GNC platform is a fully integrated, flight-proven system combining all sensors, actuators, and control software required for precise spacecraft attitude and orbit control. &nbsp;Built exclusively from Space Inventor hardware and software, this modular suite offers a complete in-house solution that can be tailored to meet diverse mission requirements — from agile CubeSats to high-precision MicroSats operating in LEO, MEO, or GEO.&nbsp;\u003Cbr>\u003Cbr>At its core, the GNC Solution uses the AOCS Computer (OBC-P4) running advanced Space Inventor algorithms for sensor fusion, guidance, and closed-loop control, ensuring robust performance and high reliability in orbit. &nbsp;\u003Cbr>\u003Cbr>The number, type, and configuration of sensors and actuators are fully customizable and selected according to each mission’s specific requirements and objectives.&nbsp;\u003C\u002Fp>\u003Cp class=\"p1\">&nbsp;\u003C\u002Fp>","page-components.rich-text",{"id":188,"media":207,"__component":265},[208],{"id":209,"name":210,"alternativeText":15,"caption":15,"width":211,"height":212,"formats":213,"hash":259,"ext":96,"mime":97,"size":260,"url":261,"previewUrl":15,"provider":100,"provider_metadata":15,"createdAt":262,"updatedAt":262,"documentId":263,"publishedAt":264,"focalPoint":15},590,"GNC.png",2657,845,{"large":214,"small":222,"medium":229,"xlarge":237,"xsmall":245,"thumbnail":252},{"ext":96,"url":215,"hash":216,"mime":97,"name":217,"path":15,"size":218,"width":219,"height":220,"sizeInBytes":221},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Flarge_GNC_910db97511.png","large_GNC_910db97511","large_GNC.png",109.32,1024,326,109318,{"ext":96,"url":223,"hash":224,"mime":97,"name":225,"path":15,"size":226,"width":123,"height":227,"sizeInBytes":228},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fsmall_GNC_910db97511.png","small_GNC_910db97511","small_GNC.png",35.92,159,35921,{"ext":96,"url":230,"hash":231,"mime":97,"name":232,"path":15,"size":233,"width":234,"height":235,"sizeInBytes":236},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fmedium_GNC_910db97511.png","medium_GNC_910db97511","medium_GNC.png",70.95,768,244,70953,{"ext":96,"url":238,"hash":239,"mime":97,"name":240,"path":15,"size":241,"width":242,"height":243,"sizeInBytes":244},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fxlarge_GNC_910db97511.png","xlarge_GNC_910db97511","xlarge_GNC.png",304.05,1920,611,304051,{"ext":96,"url":246,"hash":247,"mime":97,"name":248,"path":15,"size":249,"width":131,"height":250,"sizeInBytes":251},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fxsmall_GNC_910db97511.png","xsmall_GNC_910db97511","xsmall_GNC.png",16.26,95,16258,{"ext":96,"url":253,"hash":254,"mime":97,"name":255,"path":15,"size":256,"width":139,"height":257,"sizeInBytes":258},"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fthumbnail_GNC_910db97511.png","thumbnail_GNC_910db97511","thumbnail_GNC.png",11.95,78,11951,"GNC_910db97511",90.79,"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002FGNC_910db97511.png","2026-02-06T09:21:28.373Z","gxkwpg0hnd0up4m2auxhz62j","2026-02-06T09:21:28.374Z","page-components.full-width-media",{"id":267,"content":268,"contentLeft":269,"backgroundColor":270,"textColor":271,"media":15,"__component":272},56,"\u003Ch3 class=\"gradient-text\" style=\"text-align:center;\">Core Functionality\u003C\u002Fh3>\u003Cp style=\"text-align:center;\">\u003Cstrong>Attitude Determination\u003C\u002Fstrong>&nbsp;\u003Cbr>Fused data from star trackers, IMU, magnetometers, and FSS modules using advanced Extended Kalman Filtering &nbsp;\u003Cbr>\u003Cbr>\u003Cstrong>Attitude Control Modes\u003C\u002Fstrong>&nbsp;\u003Cbr>The systems provides &nbsp;precision control using reaction wheels for fine maneuvers and magnetorquers for momentum management as well as several advanced control modes: Nadir, Velocity, ECI, Safe sun pointing, Sun pointing with tertiary pointing target, bore axis pointing with tertiary axis sun optimized, inertial pointing, limb tracking, target tracking, ground station tracking, push broom imaging mode\u003Cbr>\u003Cbr>\u003Cstrong>Orbit Determination\u003C\u002Fstrong>&nbsp;\u003Cbr>GNSS-based position and velocity tracking with integrated guidance algorithms &nbsp;\u003Cbr>\u003Cbr>\u003Cstrong>Momentum Management\u003C\u002Fstrong>&nbsp;\u003Cbr>Automatic unloading of wheel momentum using magnetorquer rods or propulsion system &nbsp;\u003Cbr>\u003Cbr>\u003Cstrong>Fault Tolerance\u003C\u002Fstrong>&nbsp;\u003Cbr>Hierarchical State Machine and FDIR framework provide autonomous fault detection and recovery\u003C\u002Fp>\u003Cp style=\"text-align:center;\">&nbsp;\u003C\u002Fp>",false,"#222222","#ffffff","page-components.infobox",{"id":274,"content":275,"__component":205},336,"\u003Ch3 style=\"text-align:center;\">\u003Cspan class=\"s1\">\u003Cstrong>Typical Pointing Performance\u003C\u002Fstrong>\u003C\u002Fspan>\u003C\u002Fh3>\u003Cfigure class=\"table\">\u003Ctable>\u003Ctbody>\u003Ctr>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">\u003Cspan class=\"s1\">\u003Cstrong>Platform Type\u003C\u002Fstrong>\u003C\u002Fspan>\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp style=\"text-align:center;\">\u003Cstrong>Sensor and Actuator Suite\u003C\u002Fstrong>\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp style=\"text-align:center;\">\u003Cstrong>Typical Pointing Accuracy\u003C\u002Fstrong>\u003C\u002Fp>\u003C\u002Ftd>\u003C\u002Ftr>\u003Ctr>\u003Ctd>\u003Cp style=\"text-align:center;\">\u003Cstrong>6U CubeSat\u003C\u002Fstrong>\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">WHL-P4 + FSS + IMU-P4\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">&lt; 2º\u003C\u002Fp>\u003C\u002Ftd>\u003C\u002Ftr>\u003Ctr>\u003Ctd>\u003Cp style=\"text-align:center;\">\u003Cstrong>16U CubeSat\u003C\u002Fstrong>\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">STR + WHL-P4 + FSS + IMU-P4\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">0.1º - 0.5º\u003C\u002Fp>\u003C\u002Ftd>\u003C\u002Ftr>\u003Ctr>\u003Ctd>\u003Cp style=\"text-align:center;\">\u003Cstrong>Microsat 50-200 kg (Micro-8 \u002F Micro-24)\u003C\u002Fstrong>\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">Dual STR + WHL-P4 + FSS + IMU-P4\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">50 arcsec\u003C\u002Fp>\u003C\u002Ftd>\u003C\u002Ftr>\u003Ctr>\u003Ctd>\u003Cp style=\"text-align:center;\">\u003Cstrong>Precision Missions (e.g. telescopes)\u003C\u002Fstrong>\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp style=\"text-align:center;\">Dual STR + WHL-P4 + advanced calibration\u003C\u002Fp>\u003C\u002Ftd>\u003Ctd>\u003Cp class=\"p1\" style=\"text-align:center;\">Arcsecond\u003C\u002Fp>\u003Cp class=\"p1\" style=\"text-align:center;\">(with in-orbit tuning)\u003C\u002Fp>\u003C\u002Ftd>\u003C\u002Ftr>\u003C\u002Ftbody>\u003C\u002Ftable>\u003C\u002Ffigure>",{"id":277,"content":278,"contentLeft":279,"backgroundColor":271,"textColor":15,"media":15,"__component":272},57,"\u003Ch3 style=\"text-align:center;\">\u003Cspan class=\"s1\">\u003Cstrong>GNC Platform Subcomponents\u003C\u002Fstrong>\u003C\u002Fspan>\u003C\u002Fh3>",true,{"id":281,"showVerticalDivider":269,"columns":282,"__component":289},80,[283,286],{"id":284,"content":285},337,"\u003Cp>\u003Cspan style=\"font-size:18px;\">\u003Cstrong>AOCS Computer&nbsp;\u003C\u002Fstrong>\u003C\u002Fspan>\u003Cbr>The AOCS Computer and software &nbsp;(OBC-P4 + AOCS SW) is the central control unit of the GNC platform. It interfaces with all sensors and actuators via a redundant CAN bus using the CubeSat Space Protocol (CSP), managing real-time attitude and orbit control tasks.\u003Cbr>&nbsp;\u003C\u002Fp>\u003Cp>\u003Cstrong>Key features include:\u003C\u002Fstrong> &nbsp;&nbsp;&nbsp;&nbsp;\u003Cbr>Executes all AOCS and GNC software, including sensor fusion, actuator control, conops and FDIR\u003Cbr>Robust, radiation-tolerant design with independent power and data interfaces\u003Cbr>Quad-core ARM Cortex-M7 architecture for real-time parallel processing\u003Cbr>\u003Cbr>The OBC-P4 ensures coordinated and deterministic operation of all subsystems, serving as the backbone of the GNC suite. &nbsp;\u003Cbr>\u003Cbr>\u003Cspan style=\"font-size:18px;\">\u003Cstrong>Actuators\u003C\u002Fstrong>\u003C\u002Fspan>&nbsp;\u003Cbr>GNC actuators Provide precise and stable attitude control and momentum management across all spacecraft axes.&nbsp;\u003Cbr>\u003Cbr>\u003Cstrong>The platform typically includes: &nbsp;&nbsp;&nbsp;&nbsp;\u003C\u002Fstrong>\u003Cbr>Reaction Wheels (WHL-P4 series): Fine 3-axis control&nbsp;and agile slews\u003Cbr>Magnetorquer Rods (MT series): Momentum dumping and safe-mode stabilization\u003Cbr>Optional Propulsion Interface: Various 3rd party propulsion systems can be added for orbit control and advanced maneuvering&nbsp;\u003Cbr>\u003Cbr>The number and configuration of actuators are tailored to meet specific mission performance and redundancy requirements.\u003C\u002Fp>",{"id":287,"content":288},338,"\u003Cp>\u003Cspan style=\"font-size:18px;\">\u003Cstrong>Sensors\u003C\u002Fstrong>&nbsp;\u003C\u002Fspan>\u003Cbr>A number of GNC sensors &nbsp;provide accurate and reliable attitude and orbit determination across multiple operating modes.&nbsp;\u003Cbr>\u003Cbr>Typical sensor modules include:&nbsp;\u003Cbr>Star Trackers (ASTRO-CL \u002F SFC): High-precision attitude &nbsp;measurement with onboard image processing\u003Cbr>Fine Sun Sensors (FSS): Coarse attitude and Sun-pointing capability\u003Cbr>Inertial Measurement Unit (IMU-P4): Redundant gyroscopes, accelerometers, and magnetometers for continuous rate sensing\u003Cbr>GNSS Receivers (GNSS-P3): Precise position and velocity data for orbit determination &nbsp;\u003Cbr>\u003Cbr>Sensor configuration can be adapted for varying precision, redundancy, and environmental conditions. &nbsp;\u003Cbr>\u003Cbr>\u003Cspan style=\"font-size:18px;\">\u003Cstrong>Power &amp; Communication Infrastructure\u003C\u002Fstrong>&nbsp;\u003C\u002Fspan>\u003Cbr>Power Distribution Units (PDU-P4) provide regulated and redundant power to all GNC components, with latch-up protection and integrated CAN communication across the subsystem network.\u003C\u002Fp>\u003Cfigure class=\"image image_resized\" style=\"width:80.23%;\">\u003Cimg alt=\"StarTracker.png\" src=\"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002FStar_Tracker_484f1ec189.png\" srcset=\"https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fthumbnail_Star_Tracker_484f1ec189.png 198w, https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fxsmall_Star_Tracker_484f1ec189.png 300w, https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fsmall_Star_Tracker_484f1ec189.png 500w, https:\u002F\u002Fbeneficial-confidence-e608107b82.media.strapiapp.com\u002Fmedium_Star_Tracker_484f1ec189.png 768w\" sizes=\"100vw\" width=\"768\">\u003C\u002Ffigure>\u003Cp>\u003Cbr>&nbsp;\u003C\u002Fp>","page-components.row",{"id":291,"content":292,"__component":293},35,"\u003Ch3 style=\"text-align:center;\">Performance &amp; Heritage\u003C\u002Fh3>\u003Cp style=\"text-align:center;\">The system achieves arcsecond attitude determination and high-precision control, verified across flight-proven Space Inventor missions in both LEO and GEO. Its modular, distributed architecture allows rapid adaptation to spacecraft mass, inertia, and mission profile — ensuring optimal GNC performance for satellites from 10 kg &nbsp;CubeSats up to 200+ kg MicroSats.\u003Cbr>\u003Cbr>&nbsp;\u003C\u002Fp>\u003Chr>\u003Cp style=\"text-align:center;\">MSRP\u003C\u002Fp>\u003Ch3 style=\"text-align:center;\">€200.000-600.000\u003C\u002Fh3>","page-components.gradient-info-box",{"id":295,"text":296,"buttonStyle":13,"link":14,"square":15,"opacity":15,"bigFullWidth":15,"__component":297},193,"Get in Contact","components.cta",{"pagination":299},{"page":300,"pageSize":301,"pageCount":300,"total":300},1,25,1780579179710]