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Displayed error for GNSS/IMU coupling #84

Answered by rodralez
Adrienmangini asked this question in Q&A
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Hello,

The declaration of function att_update is:

[qua, DCMbn, euler] = att_update(wb, DCMbn, qua, omega_ie_n, omega_en_n, dt, att_mode)

Two attitude modes can be set: dcm and quaternion. If no att_mode is provided, the quaternion mode is the default attitude mode.

Maybe you misspelled the attitude mode, as cuaternion or dcn. In this case, no attitude mode will be set.

Kind regards.

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