Physics Asked on May 13, 2021
I’ll be using Hubert Hahn’s notation for my question. Hahn has an algebraic treatment of all values.
How would I go about calculating $G$‘s rotation relative to space-fixed frame $N$ ($omega_{GN}^{N}$)?
Since $G$‘s rotation is defined with respect to $B$ I’d argue we split $omega_{GN}^G$ like so
$$omega_{GN}^G = omega_{GB}^G + omega_{BN}^G =omega_{GB}^G + A^{GB}omega_{BN}^B $$
I worry I’m missing out on the kinematic attitude treatment.
According to Hahn: $dot{eta} = H(eta)cdot omega^R_{LR} = H(eta)cdot A^{RL} cdot omega^L_{LR}$,
where $H(eta)$ is the kinematic attitude matrix.
thus:
@JAlex Answered the question in the comments. $eta$ is NOT a cartesian vector. The attitude matrix converts a cartesian angular rate of the rotating frame (say $omega_{BN}^{N}$) to the rigid-body-orientation-parameter-representation rate of change $dot{eta}$! I call them parameters because their derivative ($dot{eta}$) is not to be confused with an angular velocity. It is more related to the derivative of the transformation matrix, like JAlex points out:
$$ dot{A}^{BN} = omega_{BN}^{B} times A^{BN} $$
My mind is blown. I had read many rigid body related documents but none were clear on this matter.
Correct answer by FemtoComm on May 13, 2021
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