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    The study of gravity gradient effect on attitude of low earth orbit satellite

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    The study of gravity gradient effect on attitude of low earth orbit satellite.pdf (9.357Kb)
    Date
    2013
    Author
    Nor Hazadura, Hamzah
    Sazali, Yaacob, Prof. Dr.
    Hariharan, Muthusamy, Dr.
    Norhizam, Hamzah
    Najah, Ghazali
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    Abstract
    Simulations and mathematical models are increasingly used to assist the process of decision making in engineering design. The objective of this paper is to simulate the linear attitude dynamics of small satellites under gravity gradient torque which is inherent in low earth orbit. The equations were first derived in their nonlinear form, and then manipulated and simulated in their linear form. Simulation results demonstrate the importance of choosing the appropriate values of satellite's moment of inertia in designing phase of a satellite.
    URI
    http://scitation.aip.org/content/aip/proceeding/aipcp/10.1063/1.4801184
    http://dspace.unimap.edu.my:80/dspace/handle/123456789/34179
    Collections
    • School of Mechatronic Engineering (Articles) [319]
    • Institute of Engineering Mathematics (Articles) [74]
    • Hariharan Muthusamy, Dr. [77]
    • Sazali Yaacob, Prof. Dr. [250]

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