Design & computational analysis for satellite attitude control systems and perturbation correction analysis for nanosatellites in low earth orbit with utilization of kalman filters

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dc.contributor.authorM, Raja
dc.date.accessioned2021-02-23T12:04:50Z
dc.date.available2021-02-23T12:04:50Z
dc.date.issued2019-02
dc.identifier.urihttp://hdl.handle.net/123456789/2986
dc.language.isoenen_US
dc.publisherUPES, Dehradunen_US
dc.subjectAerospace Engineeringen_US
dc.subjectSatellite Control Systemsen_US
dc.subjectNanosatelliteen_US
dc.titleDesign & computational analysis for satellite attitude control systems and perturbation correction analysis for nanosatellites in low earth orbit with utilization of kalman filtersen_US
dc.typeThesisen_US

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