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Please use this identifier to cite or link to this item: http://20.198.91.3:8080/jspui/handle/123456789/9347
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DC FieldValueLanguage
dc.contributor.advisorSadhu (Ghosh), Smita-
dc.contributor.authorMandal, Ayandeep-
dc.date.accessioned2026-01-07T07:08:44Z-
dc.date.available2026-01-07T07:08:44Z-
dc.date.issued2024-
dc.date.submitted2024-
dc.identifier.otherDC3872-
dc.identifier.urihttp://20.198.91.3:8080/jspui/handle/123456789/9347-
dc.format.extent79p.en_US
dc.language.isoenen_US
dc.publisherJadavpur University, Kolkata, West Bengalen_US
dc.subjectSensors and Actuatorsen_US
dc.subjectAttitude Control Techniques for Microen_US
dc.subjectNano Satellitesen_US
dc.subjectEuler Angle-based Mathematical Modelen_US
dc.titleDifferent approaches of modelling and attitude control of microsatellite with inertial coupling in presence of disturbanceen_US
dc.typeTexten_US
dc.departmentJadavpur University, Dept. of Control System Engineeringen_US
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