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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.author | M, Raja | |
| dc.date.accessioned | 2021-02-23T12:04:50Z | |
| dc.date.available | 2021-02-23T12:04:50Z | |
| dc.date.issued | 2019-02 | |
| dc.identifier.uri | http://hdl.handle.net/123456789/2986 | |
| dc.language.iso | en | en_US |
| dc.publisher | UPES, Dehradun | en_US |
| dc.subject | Aerospace Engineering | en_US |
| dc.subject | Satellite Control Systems | en_US |
| dc.subject | Nanosatellite | en_US |
| dc.title | Design & computational analysis for satellite attitude control systems and perturbation correction analysis for nanosatellites in low earth orbit with utilization of kalman filters | en_US |
| dc.type | Thesis | en_US |
