174 lines
7.6 KiB
Markdown
174 lines
7.6 KiB
Markdown
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title = "Dynamic modeling of flexure jointed hexapods for control purposes"
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author = ["Thomas Dehaeze"]
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draft = false
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### Backlinks {#backlinks}
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- [Identification and decoupling control of flexure jointed hexapods]({{< relref "chen00_ident_decoup_contr_flexur_joint_hexap" >}})
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Tags
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: [Stewart Platforms]({{< relref "stewart_platforms" >}}), [Flexible Joints]({{< relref "flexible_joints" >}})
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Reference
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: ([McInroy 1999](#org5efb28a))
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Author(s)
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: McInroy, J.
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Year
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: 1999
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This conference paper has been further published in a journal as a short note ([McInroy 2002](#org4990a96)).
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## Abstract {#abstract}
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> This paper presents a new dynamic model suitable for control of flexure jointed hexapods (FJH).
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>
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> Novel contributions include:
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>
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> 1. Base acceleration inputs are included
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> 2. The dynamic model is experimentally verified
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> 3. The model is developed so that it is suitable for control
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> 4. A decoupled force control is derived
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## Strut Dynamics {#strut-dynamics}
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The actuators for FJHs can be divided into two categories:
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1. soft (voice coil), which employs a spring flexure mount
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2. hard (piezoceramic or magnetostrictive), which employs a compressive load spring.
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<a id="org5279430"></a>
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{{< figure src="/ox-hugo/mcinroy99_general_hexapod.png" caption="Figure 1: A general Stewart Platform" >}}
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Since both actuator types employ force production in parallel with a spring, they can both be modeled as shown in Figure [2](#org6b356c7).
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In order to provide low frequency passive vibration isolation, the hard actuators are sometimes placed in series with additional passive springs.
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<a id="org6b356c7"></a>
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{{< figure src="/ox-hugo/mcinroy99_strut_model.png" caption="Figure 2: The dynamics of the i'th strut. A parallel spring, damper and actuator drives the moving mass of the strut and a payload" >}}
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<a id="table--tab:mcinroy99-strut-model"></a>
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<div class="table-caption">
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<span class="table-number"><a href="#table--tab:mcinroy99-strut-model">Table 1</a></span>:
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Definition of quantities on Figure <a href="#org6b356c7">2</a>
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</div>
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| **Symbol** | **Meaning** |
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|------------------------------|--------------------------------------------|
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| \\(m\_i\\) | moving strut mass |
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| \\(k\_i\\) | spring constant |
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| \\(b\_i\\) | damping constant |
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| \\(f\_m\\) | force the actuator applies |
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| \\(f\_{p\_i}\\) | forced exerted by the payload |
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| \\(p\_i\\) | three dimensional position of the top |
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| \\(q\_i\\) | three dimensional position of the bottom |
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| \\(l\_i\\) | strut length |
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| \\(l\_{r\_i}\\) | relaxed strut length |
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| \\(v\_i = p\_i - q\_i\\) | vector pointing from the bottom to the top |
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| \\(\hat{u}\_i = v\_i/l\_i\\) | unit direction of the strut |
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It is here supposed that \\(f\_{p\_i}\\) is predominantly in the strut direction (explained in ([McInroy 2002](#org4990a96))).
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This is a good approximation unless the spherical joints and extremely stiff or massive, of high inertia struts are used.
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This allows to reduce considerably the complexity of the model.
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From Figure [2](#org6b356c7) (b), forces along the strut direction are summed to yield (projected along the strut direction, hence the \\(\hat{u}\_i^T\\) term):
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\begin{equation}
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m\_i \hat{u}\_i^T \ddot{p}\_i = f\_{m\_i} - f\_{p\_i} - m\_i \hat{u}\_i^Tg - k\_i(l\_i - l\_{r\_i}) - b\_i \dot{l}\_i
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\end{equation}
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The acceleration \\(\hat{u}\_i^T \ddot{p}\_i\\) can be written as:
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\\[ \hat{u}\_i^T \ddot{p}\_i = \ddot{l}\_i + \hat{u}\_i^T \ddot{q}\_i - \dot{\hat{u}}\_i^T \dot{v}\_i \\]
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- [ ] Not sure how the last term is obtained
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Separating strut and base accelerations, and putting all six strut equations in a single vector yields:
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\begin{equation}
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f\_p = f\_m - M\_s \ddot{l} - B \dot{l} - K(l - l\_r) - M\_s \ddot{q}\_u - M\_s g\_u + M\_s v\_2 \label{eq:strut\_dynamics\_vec}
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\end{equation}
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where:
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- \\(\ddot{q}\_u = \left[ \hat{u}\_1^T \ddot{q}\_1 \ \dots \ \hat{u}\_6^T \ddot{q}\_6 \right]^T\\) notes the vector of base accelerations in the strut directions
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- \\(g\_u\\) denotes the vector of gravity accelerations in the strut directions
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- \\(Ms = \diag([m\_1\ \dots \ m\_6])\\), \\(f\_p = [f\_{p\_1}\ \dots \ f\_{p\_6}]^T\\)
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- \\(v\_2 = [ \dot{\hat{u}}\_1^T \dot{v}\_1 \ \dots \ \dot{\hat{u}}\_6^T \dot{v}\_6 ]^T\\)
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## Payload Dynamics {#payload-dynamics}
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The payload is modeled as a rigid body:
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\begin{equation}
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\underbrace{\begin{bmatrix}
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m I\_3 & 0\_{3\times 3} \\\\\\
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0\_{3\times 3} & {}^cI
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\end{bmatrix}}\_{M\_x} \ddot{\mathcal{X}} + \underbrace{\begin{bmatrix}
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0\_{3 \times 1} \\ \omega \times {}^cI\omega
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\end{bmatrix}}\_{c(\omega)} = \mathcal{F} \label{eq:payload\_dynamics}
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\end{equation}
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where:
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- \\(\ddot{\mathcal{X}}\\) is the \\(6 \times 1\\) generalized acceleration of the payload's center of mass
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- \\(\omega\\) is the \\(3 \times 1\\) payload's angular velocity vector
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- \\(\mathcal{F}\\) is the \\(6 \times 1\\) generalized force exerted on the payload
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- \\(M\_x\\) is the combined mass/inertia matrix of the payload, written in the payload frame {P}
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- \\(c(\omega)\\) represents the shown vector of Coriolis and centripetal terms
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Note \\(\dot{\mathcal{X}} = [\dot{p}^T\ \omega^T]^T\\) denotes the time derivative of the payload's combined position and orientation (or pose) with respect to a universal frame of reference {U}.
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First, consider the **generalized force due to struts**.
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Denoting this force as \\(\mathcal{F}\_s\\), it can be calculated form the strut forces as:
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\begin{equation}
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\mathcal{F}\_s = {}^UJ^T f\_p = {}^U\_BR J^T f\_p
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\end{equation}
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where \\(J\\) is the manipulator Jacobian and \\({}^U\_BR\\) is the rotation matrix from {B} to {U}.
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The total generalized force acting on the payload is the sum of the strut, exogenous, and gravity forces:
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\begin{equation}
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\mathcal{F} = {}^UJ^T f\_p + \mathcal{F}\_e - \begin{bmatrix} mg \\ 0\_{3\times 1} \end{bmatrix} \label{eq:generalized\_force}
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\end{equation}
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where:
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- \\(\mathcal{F}\_e\\) represents a vector of exogenous generalized forces applied at the center of mass
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- \\(g\\) is the gravity vector
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By combining \eqref{eq:strut_dynamics_vec}, \eqref{eq:payload_dynamics} and \eqref{eq:generalized_force}, a single equation describing the dynamics of a flexure jointed hexapod can be found:
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\begin{aligned}
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& {}^UJ^T [ f\_m - M\_s \ddot{l} - B \dot{l} - K(l - l\_r) - M\_s \ddot{q}\_u\\\\\\
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& - M\_s g\_u + M\_s v\_2] + \mathcal{F}\_e - \begin{bmatrix} mg \\ 0\_{3\times 1} \end{bmatrix} = M\_x \ddot{\mathcal{X}} + c(\omega)
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\end{aligned}
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Joint (\\(l\\)) and Cartesian (\\(\mathcal{X}\\)) terms are still mixed.
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In the next section, a connection between the two will be found to complete the formulation
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## Relationships between joint and cartesian space {#relationships-between-joint-and-cartesian-space}
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## Joint Space Dynamics {#joint-space-dynamics}
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## Control Example {#control-example}
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## Bibliography {#bibliography}
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<a id="org5efb28a"></a>McInroy, J.E. 1999. “Dynamic Modeling of Flexure Jointed Hexapods for Control Purposes.” In _Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328)_, nil. <https://doi.org/10.1109/cca.1999.806694>.
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<a id="org4990a96"></a>———. 2002. “Modeling and Design of Flexure Jointed Stewart Platforms for Control Purposes.” _IEEE/ASME Transactions on Mechatronics_ 7 (1):95–99. <https://doi.org/10.1109/3516.990892>.
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