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Fixed rotation matrix to roll-pitch-yaw conversion to comply with the following roll-pitch-yaw definition:
R_ref_body = Rz(yaw)*Ry(pitch)*Rx(roll) // body w.r.t. reference frame
where Ri denotes the rotation around axis i.

Additional info on orientation of coordinate frames:
https://en.wikipedia.org/wiki/Aircraft_principal_axes#/media/File:Yaw_Axis_Corrected.svg

Thanks, @radfordi!

Fixed rotation matrix to roll-pitch-yaw conversion to comply with the following roll-pitch-yaw definition:
R_ref_body = Rz(yaw)*Ry(pitch)*Rx(roll) // body w.r.t. reference frame
where Ri denotes the rotation around axis i.

Additional info on orientation of coordinate frames:
https://en.wikipedia.org/wiki/Aircraft_principal_axes#/media/File:Yaw_Axis_Corrected.svg

Thanks, @radfordi!
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@radfordi radfordi left a comment

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Thanks @schmidtp1. I think this should be targeted towards development not master.

@schmidtp1 schmidtp1 changed the base branch from master to development May 28, 2019 20:25
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@ev-mp ev-mp left a comment

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Thanks @schmidtp1

@ev-mp ev-mp merged commit e8380a5 into IntelRealSense:development May 30, 2019
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3 participants