IR@JU Digital Repository
IR@JU preserves and enables easy and open access to all types of digital content including text, images, moving images, mpegs and data sets
Learn More
Please use this identifier to cite or link to this item:
http://20.198.91.3:8080/jspui/handle/123456789/9347| Title: | Different approaches of modelling and attitude control of microsatellite with inertial coupling in presence of disturbance |
| Authors: | Mandal, Ayandeep |
| Advisors: | Sadhu (Ghosh), Smita |
| Keywords: | Sensors and Actuators;Attitude Control Techniques for Micro;Nano Satellites;Euler Angle-based Mathematical Model |
| Issue Date: | 2024 |
| Publisher: | Jadavpur University, Kolkata, West Bengal |
| URI: | http://20.198.91.3:8080/jspui/handle/123456789/9347 |
| Appears in Collections: | Dissertations |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| M.Tech (Department of Control System Engineering) Ayandeep Mandal.pdf | 2.42 MB | Adobe PDF | View/Open |
Items in IR@JU are protected by copyright, with all rights reserved, unless otherwise indicated.