EphemerisMsgPayload#
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struct EphemerisMsgPayload#
Message structure used to write ephemeris states out to other modules.
Public Members
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double r_BdyZero_N[3]#
[m] Position of orbital body
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double v_BdyZero_N[3]#
[m/s] Velocity of orbital body
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double sigma_BN[3]#
MRP attitude of the orbital body fixed frame relative to inertial.
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double omega_BN_B[3]#
[r/s] angular velocity of the orbital body relative to inertial
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double timeTag#
[s] vehicle Time-tag for state
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double r_BdyZero_N[3]#