Please use this identifier to cite or link to this item: https://dr.ddn.upes.ac.in//xmlui/handle/123456789/2986
Title: Design & computational analysis for satellite attitude control systems and perturbation correction analysis for nanosatellites in low earth orbit with utilization of kalman filters
Authors: M, Raja
Keywords: Aerospace Engineering
Satellite Control Systems
Nanosatellite
Issue Date: Feb-2019
Publisher: UPES, Dehradun
URI: http://hdl.handle.net/123456789/2986
Appears in Collections:Thesis

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