1. Shodhganga@INFLIBNET
  2. University of Petroleum and Energy Studies (UPES)
  3. Department of Aerospace Engineering
Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/282844
Title: Design And Computational Analysis For Satellite Attitude Control Systems And Perturbation Correction Analysis For Nanosatellites In Low Earth Orbit With Utilization Of Kalman Filters
Researcher: Raja, M
Guide(s): Guven, Ugur ,Prakash Om ,
Keywords: Computational Analysis
Engineering and Technology,Engineering,Engineering Aerospace
University: University of Petroleum and Energy Studies (UPES)
Completed Date: 2019
Abstract: newline As Attaachment
Pagination: 233
URI: http://hdl.handle.net/10603/282844
Appears in Departments:Department of Aerospace Engineering

Files in This Item:
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01_title.pdfAttached File74.73 kBAdobe PDFView/Open
02_acknowledgement.pdf91.11 kBAdobe PDFView/Open
03_declaration.pdf111.61 kBAdobe PDFView/Open
04_dedicated.pdf40.61 kBAdobe PDFView/Open
05_certificate.pdf680.23 kBAdobe PDFView/Open
06_abstract.pdf109.79 kBAdobe PDFView/Open
07_table of contents.pdf143.2 kBAdobe PDFView/Open
08_list of abbrevieation.pdf69.05 kBAdobe PDFView/Open
09_list of symbols.pdf151.91 kBAdobe PDFView/Open
10_ list of figures.pdf147.24 kBAdobe PDFView/Open
11_list of tables.pdf117.18 kBAdobe PDFView/Open
12_chapter 1.pdf164.16 kBAdobe PDFView/Open
13_chapter 2.pdf206.51 kBAdobe PDFView/Open
14_chapter 3.pdf597.12 kBAdobe PDFView/Open
15_chapter 4.pdf2.57 MBAdobe PDFView/Open
16_chapter 5.pdf1.74 MBAdobe PDFView/Open
17_chapter 6.pdf2.26 MBAdobe PDFView/Open
18_chapter 7.pdf109.25 kBAdobe PDFView/Open
19_references.pdf214.45 kBAdobe PDFView/Open
20_model code.pdf142.07 kBAdobe PDFView/Open
21_appendix.pdf1.66 MBAdobe PDFView/Open
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