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    Dynamic Response Of A Satellite With Flexible Appendages And Its Passive Control 

    Joseph, Thomas K (2010-11-25)
    Most present day spacecrafts have large interconnected solar panels. The dynamic behavior of the spacecraft in orbit can be modeled as a free rigid mass with flexible elements attached to it. The natural frequencies of ...

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    Author
    Joseph, Thomas K (1)
    SubjectArtificial Satellite - Dynamics (1)Artificial Satellites - Attitude Control Systems (1)
    Astronautics (1)
    Flexible Spacecraft Control (1)Passive Damping Treatment (1)Space Vehicle - Dynamics (1)Space Vehicles - Control Systems (1)Viscoelastic Layer Damping (1)... View MoreDate Issued2010 (1)Has File(s)Yes (1)

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