{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2026,7,10]],"date-time":"2026-07-10T22:37:00Z","timestamp":1783723020351,"version":"3.55.0"},"reference-count":45,"publisher":"Wiley","license":[{"start":{"date-parts":[[2022,10,7]],"date-time":"2022-10-07T00:00:00Z","timestamp":1665100800000},"content-version":"unspecified","delay-in-days":0,"URL":"https:\/\/creativecommons.org\/licenses\/by\/4.0\/"}],"content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":["Computational Intelligence and Neuroscience"],"published-print":{"date-parts":[[2022,10,7]]},"abstract":"<jats:p>The satellite communication is embellished constantly by providing information, ensuring security, and enables the communication among huge at a particular time efficiently. The satellite navigation helps in determining the people\u2019s location. Global development, natural disasters, change in climatic conditions, agriculture crop growth, etc., are monitored using satellite observation. Hence, the satellite includes detailed information data, and it must be protected confidentially. The field of the satellite is enhanced at an astonishing pace. Satellite data play an important role in this modern world; hence, the onboard-satellite data must secure through the proper selection of error detection and estimation schema. Lightweight deep learning algorithm based on Extended Kalman Filter (KFK) is proposed to detect and estimate onboard pointing error such as an error in attitude and orbit. The Extended Kalman Filter (EKF) is widely used in the satellite system. EKF is utilized in this proposed model to detect the onboard pointing error such as attitude and orbit determination. An autonomous estimation of orbit position is possible through space-borne gravity. The information obtained through the observation of satellite data is compared with the accurate gravity model in detecting the error. The utilization of EKF reduces the dependence of the ground tracking system in satellite determination. The orbital altitude and orbital position are the most important challenges faced in the satellite determination system. The satellite model using the Extended Kalman Filter is an optimum method in estimating the orbital parameters. The errors in the linearization process are detected, and this can be overcome through the proper selection of linear expansion point with the EKF algorithmic model with the Jacobian matrix calculation. The results show that the EKF implementation helps in attaining better accuracy than other methodologies. Its contribution is enormous to many space missions, autonomous rendezvous and docking for manned and unmanned missions (e.g., ISS operations and beyond, in-orbit servicing, and in-orbit refueling), routine satellite OD operations, orbital debris removal systems, Space Situational Awareness (SSA) operations, and others.<\/jats:p>","DOI":"10.1155\/2022\/4340897","type":"journal-article","created":{"date-parts":[[2022,10,7]],"date-time":"2022-10-07T17:20:34Z","timestamp":1665163234000},"page":"1-8","source":"Crossref","is-referenced-by-count":34,"title":["Onboard Pointing Error Detection and Estimation of Observation Satellite Data Using Extended Kalman Filter"],"prefix":"10.1155","volume":"2022","author":[{"ORCID":"https:\/\/orcid.org\/0000-0003-0233-5202","authenticated-orcid":true,"given":"R.","family":"Dhanalakshmi","sequence":"first","affiliation":[{"name":"Department of Computer Science and Engineering, KCG College of Technology, Karapakkam, Chennai 600 097, Tamilnadu, India"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"N. P. G.","family":"Bhavani","sequence":"additional","affiliation":[{"name":"Department of Electronics and Communication Engineering, Saveetha School of Engineering, Saveetha Institute of Medical and Technical Sciences, Chennai 602105, Tamilnadu, India"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"S. Srinivasulu","family":"Raju","sequence":"additional","affiliation":[{"name":"Department of Electronics and Instrumentation Engineering, VR Siddhartha Engineering College, Vijayawada, Andhra Pradesh, India"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0002-3643-0753","authenticated-orcid":true,"given":"Pundru Chandra","family":"Shaker Reddy","sequence":"additional","affiliation":[{"name":"School of Computing and Information Technology, REVA University, Bengaluru, Karnataka, India"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0001-5424-9600","authenticated-orcid":true,"given":"Dinesh","family":"Mavaluru","sequence":"additional","affiliation":[{"name":"Department of Information Technology, College of Computing and Informatics, Saudi Electronic University, Riyadh, Saudi Arabia"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"given":"Devesh Pratap","family":"Singh","sequence":"additional","affiliation":[{"name":"Department of Computer Science & Engineering, Graphic Era Deemed to Be University, Dehradun 248002, Uttarakhand, India"}],"role":[{"vocabulary":"crossref","role":"author"}]},{"ORCID":"https:\/\/orcid.org\/0000-0001-7556-2022","authenticated-orcid":true,"given":"Areda","family":"Batu","sequence":"additional","affiliation":[{"name":"Department of Chemical Engineering, College of Biological and Chemical Engineering, Addis Ababa Science and Technology University, Addis Ababa, Ethiopia"}],"role":[{"vocabulary":"crossref","role":"author"}]}],"member":"311","reference":[{"key":"1","first-page":"1188","article-title":"Particle filtering for gyroless attitude\/angular rate estimation algorithm","author":"Y Yafei"},{"key":"2","doi-asserted-by":"publisher","DOI":"10.1155\/2022\/1671829"},{"key":"3","doi-asserted-by":"publisher","DOI":"10.31436\/iiumej.v23i1.1822"},{"key":"4","doi-asserted-by":"publisher","DOI":"10.1155\/2022\/7252791"},{"key":"5","doi-asserted-by":"publisher","DOI":"10.1109\/wcica.2012.6359176"},{"key":"6","volume-title":"An Attitude Control System and Commissioning Results of the Snap-1 Nanosatellite","author":"W. H Steyn","year":"2000"},{"key":"7","doi-asserted-by":"publisher","DOI":"10.1016\/j.compeleceng.2022.108255"},{"key":"8","doi-asserted-by":"publisher","DOI":"10.1016\/s0273-1177(02)00298-3"},{"key":"9","doi-asserted-by":"publisher","DOI":"10.2174\/2210327910666191218124350"},{"issue":"3","key":"10","first-page":"334","article-title":"Implications of the applications of recursive least squares algorithms to satellite orbit determination using GPS measurements","volume":"8","author":"P. Pardal","year":"2009","journal-title":"WSEAS Transactions on Systems"},{"key":"11","doi-asserted-by":"publisher","DOI":"10.1007\/s11063-021-10679-4"},{"key":"12","doi-asserted-by":"publisher","DOI":"10.1029\/97jc03179"},{"key":"13","doi-asserted-by":"publisher","DOI":"10.1086\/380188"},{"key":"14","doi-asserted-by":"publisher","DOI":"10.1155\/2022\/8244176"},{"key":"15","doi-asserted-by":"publisher","DOI":"10.1016\/j.ast.2005.01.003"},{"key":"16","doi-asserted-by":"publisher","DOI":"10.1007\/s11277-017-5157-4"},{"key":"17","doi-asserted-by":"publisher","DOI":"10.1007\/s00190-008-0281-2"},{"issue":"2","key":"18","first-page":"77","article-title":"Malicious node detection system for mobile ad hoc networks","volume":"1","author":"A. Rajaram","year":"2010","journal-title":"International Journal of Computer Science and Information Technologies"},{"key":"19","doi-asserted-by":"publisher","DOI":"10.1002\/grl.50138"},{"key":"20","volume-title":"Global Positioning System (GPS) Autonomous Navigation\u201d","author":"M. P. Ananda","year":"1990"},{"key":"21","first-page":"24","article-title":"John, \u201cHighlights of GPS II-R autonomous navigation","author":"A. Rajan"},{"key":"22","doi-asserted-by":"publisher","DOI":"10.1007\/978-3-642-29175-3_30"},{"key":"23","doi-asserted-by":"publisher","DOI":"10.1115\/1.3662552"},{"key":"24","doi-asserted-by":"publisher","DOI":"10.1007\/s12083-019-00824-1"},{"key":"25","doi-asserted-by":"publisher","DOI":"10.1115\/1.3425006"},{"key":"26","first-page":"24","article-title":"Toward decimeter-level real-time orbit determination: a demonstration using the SAC-C and CHAMP Spacecraft","author":"A. Reichert"},{"key":"27","doi-asserted-by":"publisher","DOI":"10.1016\/j.asr.2007.02.062"},{"key":"28","doi-asserted-by":"publisher","DOI":"10.1007\/s00190-013-0611-x"},{"key":"29","doi-asserted-by":"publisher","DOI":"10.2514\/3.20302"},{"key":"30","doi-asserted-by":"publisher","DOI":"10.1109\/jproc.2003.823141"},{"key":"31","doi-asserted-by":"publisher","DOI":"10.5120\/9792-4375"},{"key":"32","doi-asserted-by":"publisher","DOI":"10.1088\/1757-899x\/994\/1\/012031"},{"key":"33","doi-asserted-by":"publisher","DOI":"10.1080\/03772063.2021.1920848"},{"key":"34","doi-asserted-by":"publisher","DOI":"10.1088\/0957-0233\/19\/9\/095203"},{"key":"35","doi-asserted-by":"publisher","DOI":"10.1016\/j.actaastro.2009.08.029"},{"key":"36","first-page":"891","article-title":"REFK and RUFK development for pico satellite attitude estimation in the presence of measurement faults","author":"H. E. Soken"},{"key":"37","first-page":"559","article-title":"On Board Pointing Error Detection and Estimation of Observation Satellite Data Using Extended Kalman Filter","author":"D. Ec","year":"2021"},{"issue":"34","key":"38","first-page":"817","article-title":"Efficient path reassessment based on node probability in wireless sensor network","volume":"2016","author":"C. R. Rathish","year":"2016","journal-title":"International Journal of Control Theory and Applications"},{"key":"39","doi-asserted-by":"publisher","DOI":"10.1155\/2022\/6489185"},{"issue":"7","key":"40","first-page":"16521","article-title":"Hierarchical load balanced routing protocol for wireless sensor networks","volume":"10","author":"C. R. Rathish","year":"2015","journal-title":"International Journal of Applied Engineering Research"},{"key":"41","doi-asserted-by":"publisher","DOI":"10.1166\/jctn.2017.6849"},{"key":"42","doi-asserted-by":"publisher","DOI":"10.1088\/1757-899x\/994\/1\/012031"},{"key":"43","doi-asserted-by":"publisher","DOI":"10.1155\/2022\/1128717"},{"key":"44","doi-asserted-by":"publisher","DOI":"10.1155\/2021\/8533995"},{"key":"45","doi-asserted-by":"publisher","DOI":"10.1155\/2022\/1570604"}],"container-title":["Computational Intelligence and Neuroscience"],"original-title":[],"language":"en","link":[{"URL":"http:\/\/downloads.hindawi.com\/journals\/cin\/2022\/4340897.pdf","content-type":"application\/pdf","content-version":"vor","intended-application":"text-mining"},{"URL":"http:\/\/downloads.hindawi.com\/journals\/cin\/2022\/4340897.xml","content-type":"application\/xml","content-version":"vor","intended-application":"text-mining"},{"URL":"http:\/\/downloads.hindawi.com\/journals\/cin\/2022\/4340897.pdf","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2022,11,22]],"date-time":"2022-11-22T05:57:20Z","timestamp":1669096640000},"score":1,"resource":{"primary":{"URL":"https:\/\/www.hindawi.com\/journals\/cin\/2022\/4340897\/"}},"subtitle":[],"editor":[{"given":"Vijay","family":"Kumar","sequence":"additional","affiliation":[],"role":[{"vocabulary":"crossref","role":"editor"}]}],"short-title":[],"issued":{"date-parts":[[2022,10,7]]},"references-count":45,"alternative-id":["4340897","4340897"],"URL":"https:\/\/doi.org\/10.1155\/2022\/4340897","relation":{},"ISSN":["1687-5273","1687-5265"],"issn-type":[{"value":"1687-5273","type":"electronic"},{"value":"1687-5265","type":"print"}],"subject":[],"published":{"date-parts":[[2022,10,7]]}}}