digital-brain/content/article/mcinroy99_dynam.md

+++
title = "Dynamic modeling of flexure jointed hexapods for control purposes"
author = ["Thomas Dehaeze"]
draft = false
+++

Tags
: [Stewart Platforms]({{< relref "stewart_platforms" >}}), [Flexible Joints]({{< relref "flexible_joints" >}})

Reference
: <sup id="5da427f78c552aa92cd64c2a6df961f1"><a class="reference-link" href="#mcinroy99_dynam" title="McInroy, Dynamic modeling of flexure jointed hexapods for control  purposes, nil, in in: {Proceedings of the 1999 IEEE International Conference on
                      Control Applications (Cat. No.99CH36328)}, edited by (1999)">(McInroy, 1999)</a></sup>

Author(s)
: McInroy, J.

Year
: 1999

This conference paper has been further published in a journal as a short note <sup id="8bfe2d2dce902a584fa016e86a899044"><a class="reference-link" href="#mcinroy02_model_desig_flexur_joint_stewar" title="McInroy, Modeling and Design of Flexure Jointed Stewart Platforms  for Control Purposes, {IEEE/ASME Transactions on Mechatronics}, v(1), 95-99 (2002).">(McInroy, 2002)</a></sup>.


## Abstract {#abstract}

> This paper presents a new dynamic model suitable for control of flexure jointed hexapods (FJH).
>
> Novel contributions include:
>
> 1.  Base acceleration inputs are included
> 2.  The dynamic model is experimentally verified
> 3.  The model is developed so that it is suitable for control
> 4.  A decoupled force control is derived


## Strut Dynamics {#strut-dynamics}

The actuators for FJHs can be divided into two categories:

1.  soft (voice coil), which employs a spring flexure mount
2.  hard (piezoceramic or magnetostrictive), which employs a compressive load spring.

<a id="orgb4329bb"></a>

{{< figure src="/ox-hugo/mcinroy99_general_hexapod.png" caption="Figure 1: A general Stewart Platform" >}}

Since both actuator types employ force production in parallel with a spring, they can both be modeled as shown in Figure [2](#org4a04030).

In order to provide low frequency passive vibration isolation, the hard actuators are sometimes placed in series with additional passive springs.

<a id="org4a04030"></a>

{{< 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" >}}

<a id="table--tab:mcinroy99-strut-model"></a>
<div class="table-caption">
  <span class="table-number"><a href="#table--tab:mcinroy99-strut-model">Table 1</a></span>:
  Definition of quantities on Figure <a href="#org4a04030">2</a>
</div>

| **Symbol**                   | **Meaning**                                |
|------------------------------|--------------------------------------------|
| \\(m\_i\\)                   | moving strut mass                          |
| \\(k\_i\\)                   | spring constant                            |
| \\(b\_i\\)                   | damping constant                           |
| \\(f\_m\\)                   | force the actuator applies                 |
| \\(f\_{p\_i}\\)              | forced exerted by the payload              |
| \\(p\_i\\)                   | three dimensional position of the top      |
| \\(q\_i\\)                   | three dimensional position of the bottom   |
| \\(l\_i\\)                   | strut length                               |
| \\(l\_{r\_i}\\)              | relaxed strut length                       |
| \\(v\_i = p\_i - q\_i\\)     | vector pointing from the bottom to the top |
| \\(\hat{u}\_i = v\_i/l\_i\\) | unit direction of the strut                |

It is here supposed that \\(f\_{p\_i}\\) is predominantly in the strut direction (explained in <sup id="8bfe2d2dce902a584fa016e86a899044"><a class="reference-link" href="#mcinroy02_model_desig_flexur_joint_stewar" title="McInroy, Modeling and Design of Flexure Jointed Stewart Platforms  for Control Purposes, {IEEE/ASME Transactions on Mechatronics}, v(1), 95-99 (2002).">(McInroy, 2002)</a></sup>).
This is a good approximation unless the spherical joints and extremely stiff or massive, of high inertia struts are used.
This allows to reduce considerably the complexity of the model.

From Figure [2](#org4a04030) (b), forces along the strut direction are summed to yield (projected along the strut direction, hence the \\(\hat{u}\_i^T\\) term):

\begin{equation}
  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
\end{equation}

The acceleration \\(\hat{u}\_i^T \ddot{p}\_i\\) can be written as:
\\[ \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 \\]

-   [ ] Not sure how the last term is obtained

Separating strut and base accelerations, and putting all six strut equations in a single vector yields:

\begin{equation}
  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}
\end{equation}

where:

-   \\(\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
-   \\(g\_u\\) denotes the vector of gravity accelerations in the strut directions
-   \\(Ms = \diag([m\_1\ \dots \ m\_6])\\), \\(f\_p = [f\_{p\_1}\ \dots \ f\_{p\_6}]^T\\)
-   \\(v\_2 = [ \dot{\hat{u}}\_1^T \dot{v}\_1 \ \dots \ \dot{\hat{u}}\_6^T \dot{v}\_6 ]^T\\)


## Payload Dynamics {#payload-dynamics}

The payload is modeled as a rigid body:

\begin{equation}
\underbrace{\begin{bmatrix}
m I\_3 & 0\_{3\times 3} \\\\\\
0\_{3\times 3}   & {}^cI
\end{bmatrix}}\_{M\_x} \ddot{\mathcal{X}} + \underbrace{\begin{bmatrix}
  0\_{3 \times 1} \\ \omega \times {}^cI\omega
\end{bmatrix}}\_{c(\omega)} = \mathcal{F} \label{eq:payload\_dynamics}
\end{equation}

where:

-   \\(\ddot{\mathcal{X}}\\) is the \\(6 \times 1\\) generalized acceleration of the payload's center of mass
-   \\(\omega\\) is the \\(3 \times 1\\) payload's angular velocity vector
-   \\(\mathcal{F}\\) is the \\(6 \times 1\\) generalized force exerted on the payload
-   \\(M\_x\\) is the combined mass/inertia matrix of the payload, written in the payload frame {P}
-   \\(c(\omega)\\) represents the shown vector of Coriolis and centripetal terms

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}.

First, consider the **generalized force due to struts**.
Denoting this force as \\(\mathcal{F}\_s\\), it can be calculated form the strut forces as:

\begin{equation}
  \mathcal{F}\_s = {}^UJ^T f\_p = {}^U\_BR J^T f\_p
\end{equation}

where \\(J\\) is the manipulator Jacobian and \\({}^U\_BR\\) is the rotation matrix from {B} to {U}.

The total generalized force acting on the payload is the sum of the strut, exogenous, and gravity forces:

\begin{equation}
  \mathcal{F} = {}^UJ^T f\_p + \mathcal{F}\_e - \begin{bmatrix} mg \\ 0\_{3\times 1} \end{bmatrix} \label{eq:generalized\_force}
\end{equation}

where:

-   \\(\mathcal{F}\_e\\) represents a vector of exogenous generalized forces applied at the center of mass
-   \\(g\\) is the gravity vector

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:

\begin{aligned}
  & {}^UJ^T [ 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] + \mathcal{F}\_e - \begin{bmatrix} mg \\ 0\_{3\times 1} \end{bmatrix} = M\_x \ddot{\mathcal{X}} + c(\omega)
\end{aligned}

Joint (\\(l\\)) and Cartesian (\\(\mathcal{X}\\)) terms are still mixed.
In the next section, a connection between the two will be found to complete the formulation


## Relationships between joint and cartesian space {#relationships-between-joint-and-cartesian-space}


## Joint Space Dynamics {#joint-space-dynamics}


## Control Example {#control-example}

# Bibliography
<a class="bibtex-entry" id="mcinroy99_dynam">McInroy, J., *Dynamic modeling of flexure jointed hexapods for control purposes*, In , Proceedings of the 1999 IEEE International Conference on Control Applications (Cat. No.99CH36328) (pp. ) (1999). : .</a> [↩](#5da427f78c552aa92cd64c2a6df961f1)

<a class="bibtex-entry" id="mcinroy02_model_desig_flexur_joint_stewar">McInroy, J., *Modeling and design of flexure jointed stewart platforms for control purposes*, IEEE/ASME Transactions on Mechatronics, *7(1)*, 95–99 (2002).  http://dx.doi.org/10.1109/3516.990892</a> [↩](#8bfe2d2dce902a584fa016e86a899044)


## Backlinks {#backlinks}

-   [Identification and decoupling control of flexure jointed hexapods]({{< relref "chen00_ident_decoup_contr_flexur_joint_hexap" >}})