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/10603/280029
Title: Design computational analysis for satellite attitude control systems and perturbation correction analysis for nanosatellites in low earth orbit with utilization of kalman filters
Researcher: M, Raja
Guide(s): Guven, Ugur and Om Prakash
Keywords: Engineering
Engineering Aerospace
Engineering and Technology
Nanosatellites
Perturbation
Utilization
University: University of Petroleum and Energy Studies (UPES)
Completed Date: 2019
Abstract: file attached
Pagination: p. 208
URI: http://hdl.handle.net/10603/280029
Appears in Departments:Department of Aerospace Engineering

Files in This Item:
File Description SizeFormat 
01_title.pdfAttached File73.82 kBAdobe PDFView/Open
02_acknowledgement.pdf64.94 kBAdobe PDFView/Open
03_declaration.pdf212.15 kBAdobe PDFView/Open
04_certificate.pdf274.08 kBAdobe PDFView/Open
05_abstract.pdf147.15 kBAdobe PDFView/Open
06_contents.pdf466.86 kBAdobe PDFView/Open
07_list of symbol.pdf254.16 kBAdobe PDFView/Open
08_list of figure and table.pdf232.22 kBAdobe PDFView/Open
09_chapter1.pdf171.92 kBAdobe PDFView/Open
10_chapter2.pdf333.95 kBAdobe PDFView/Open
11_chapter3.pdf3.1 MBAdobe PDFView/Open
12_chapter4.pdf2.76 MBAdobe PDFView/Open
13_chapter5.pdf1.14 MBAdobe PDFView/Open
14_chapter6.pdf2.22 MBAdobe PDFView/Open
15_chapter7.pdf142.87 kBAdobe PDFView/Open
16_references.pdf242.43 kBAdobe PDFView/Open
17_annexure.pdf1.45 MBAdobe PDFView/Open
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