Presentation & Recruitment - 21st April 2010

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    Measuring a Satellite Attitude

    using Radio Signals

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    What VORSat is Small Satellite

    CubeSat format

    10x10x10 cm 1 Kg

    LEO (350 Km altitude)

    Polar orbit

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    CubeSats Around the World

    CP-1, the first in a string of

    Cal Poly Cubesats.

    USU Microgravity Research Team (Utah State)

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    Why?

    Challenge from the Education Office of ESA

    Previous collaboration in the scope of STRAPLEX

    (stratospheric balloon flight program)

    Project developed by students

    Education oriented

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    Mission

    To measure the attitude from thegroundusing RF

    signals

    A

    1

    d

    D

    A1

    A2

    _ fffff

    fff

    (!

    !

    (!

    032

    02

    01

    1

    A

    A KHzf

    GHzf

    1

    45,20

    !(

    !

    321 ,, JJJPhases of the 3

    frequencies as received at

    GS, in cycles

    P

    E

    PJJJJ)(

    )()( 3221Dsend

    !!

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    Mission

    To measure the attitude from thegroundusing RF

    signals

    A1

    A2

    A

    1

    1. Phasedifferencebetweenone pair of antennas

    provides one angle of

    attitude

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    Mission

    To measure the attitude from thegroundusing RF

    signals

    A3

    A2

    A

    1

    1. Phasedifferencebetweenone pair of antennas

    provides one angle of

    attitude

    2. Other phasedifference

    gives the second angle

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    Mission

    To measure the attitude from thegroundusing RF

    signals

    1. Phasedifferencebetweenone pair of antennas

    provides one angle of

    attitude

    2. Other phasedifference

    gives is the second angle

    3. Thir d anglegivenby the

    change of angle of sight

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    Mission

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    Mission

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    Mission

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    Mission

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    Mission

    Ground Station @ FEUP

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    Architecture

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    Re-entry

    Changing thegeometry to increaseCx in

    order to adjust the reentry point

    Release of the reentry capsule

    Communicationduring/after reentry

    Splash down in the Atlantic

    & recovery

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    Whats new?

    Combination of solar panels with antennas in order to maximize

    the exposure area and energy provided.

    Patch antennas embedded in the solar cells layer during its

    production.

    Structure made of carbon fiber composite

    Reentry of a CubeSat

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    Work in progress

    VORSat principle for attitude determination has been

    proved viable with lab tests.

    First draft of hardware requirements and layout for the

    CubeSat defined.

    Capsule hardware layout TBD.

    Capsule release mechanism TBD.

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    Facilities

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    Colaborations

    DEEC DEMec

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    www.vorsat.org

    [email protected]

    I324@FEUP