Math  /  Algebra

Question- Consider a rack-and-pinion system. The rotational motion of the pinion is transformed into transitional motion of the rack
For simplicity, the spring effects are ignored Tin Tout =Jdωdt+c1ωT_{\text {in }}-T_{\text {out }}=J \frac{d \omega}{d t}+c_{1} \omega
Dr. Terek A. Tutanf
Example continued
The rotational equation is Tin Tout =Jdωdt+c1ωFc2v=mdvdt\begin{array}{l} T_{\text {in }}-T_{\text {out }}=J \frac{d \omega}{d t}+c_{1} \omega \\ F-c_{2} v=m \frac{d v}{d t} \end{array}
The transitional equation is
Using the equations And manipulating the rotational and transitional equations with the input torque, Tin, as inputs and velocity, v , as output, we get Tout =rFω=v/rTin =(c1/r+c2r)v+(J/r+mr)dvdt\begin{array}{l} T_{\text {out }}=r F \\ \omega=v / r \\ T_{\text {in }}=\left(c_{1} / r+c_{2} r\right) v+(J / r+m r) \frac{d v}{d t} \end{array} Dr. Tarek A. Tutunji
Example continued
Let us take a look at the state space equations In general, where x is the states vector, y is the output vector, and uu is the input vector
In our example, we will use the states: ω\omega and vv, the inputs: Tin\mathrm{T}_{\mathrm{in}} and F the output: v [dω/dtdv/dt]=[c1/J00c2/m][ωv]+[1/Jr/J01/m][TinF]v=[01][ωv]\begin{array}{l} {\left[\begin{array}{l} d \omega / d t \\ d v / d t \end{array}\right]=\left[\begin{array}{cc} -c_{1} / J & 0 \\ 0 & -c_{2} / m \end{array}\right]\left[\begin{array}{l} \omega \\ v \end{array}\right]+\left[\begin{array}{cc} 1 / J & -r / J \\ 0 & 1 / m \end{array}\right]\left[\begin{array}{c} T_{i n} \\ F \end{array}\right]} \\ v=\left[\begin{array}{ll} 0 & 1 \end{array}\right]\left[\begin{array}{l} \omega \\ v \end{array}\right] \end{array}

Studdy Solution

STEP 1

What is this asking? We're looking at a rack-and-pinion system and figuring out how the input torque affects the velocity of the rack, ignoring spring effects.
We'll also represent the system using state-space equations. Watch out! Don't mix up rotational and translational variables!
Also, keep track of your rr (radius) – it connects the rotational and translational worlds.

STEP 2

1. Relate Torque and Force
2. Relate Angular and Linear Velocity
3. Derive the Input-Output Relationship
4. Define State Variables
5. Construct the State-Space Representation

STEP 3

We know that torque (ToutT_{out}) applied to the pinion creates a force (FF) on the rack.
They're related by the radius (rr) of the pinion: Tout=rFT_{out} = r \cdot F

STEP 4

The angular velocity (ω\omega) of the pinion and the linear velocity (vv) of the rack are also related by the radius (rr): ω=vr\omega = \frac{v}{r}

STEP 5

We're given these two equations: TinTout=Jdωdt+c1ωT_{in} - T_{out} = J \cdot \frac{d\omega}{dt} + c_1 \cdot \omega Fc2v=mdvdtF - c_2 \cdot v = m \cdot \frac{dv}{dt}where JJ is the moment of inertia, c1c_1 and c2c_2 are damping coefficients, and mm is the mass of the rack.

STEP 6

**Substitute** the expressions for ToutT_{out} and ω\omega from the previous relationships into the first equation: TinrF=Jddt(vr)+c1vrT_{in} - r \cdot F = J \cdot \frac{d}{dt} \left( \frac{v}{r} \right) + c_1 \cdot \frac{v}{r} TinrF=Jrdvdt+c1rvT_{in} - r \cdot F = \frac{J}{r} \cdot \frac{dv}{dt} + \frac{c_1}{r} \cdot v

STEP 7

From the second given equation, we can express FF as: F=mdvdt+c2vF = m \cdot \frac{dv}{dt} + c_2 \cdot v

STEP 8

**Substitute** this expression for FF back into the equation we derived in 2.3.2: Tinr(mdvdt+c2v)=Jrdvdt+c1rvT_{in} - r \cdot \left( m \cdot \frac{dv}{dt} + c_2 \cdot v \right) = \frac{J}{r} \cdot \frac{dv}{dt} + \frac{c_1}{r} \cdot v Tinmrdvdtrc2v=Jrdvdt+c1rvT_{in} - mr \cdot \frac{dv}{dt} - rc_2 \cdot v = \frac{J}{r} \cdot \frac{dv}{dt} + \frac{c_1}{r} \cdot v

STEP 9

Now, **rearrange** the equation to isolate TinT_{in}: Tin=(Jr+mr)dvdt+(c1r+rc2)vT_{in} = \left( \frac{J}{r} + mr \right) \cdot \frac{dv}{dt} + \left( \frac{c_1}{r} + rc_2 \right) \cdot v This equation shows how the input torque (TinT_{in}) relates to the rack's velocity (vv).

STEP 10

We'll choose ω\omega and vv as our state variables, represented as a vector: x=[ωv] x = \begin{bmatrix} \omega \\ v \end{bmatrix}

STEP 11

We're given the state-space equations: dxdt=Ax+Bu\frac{dx}{dt} = Ax + Bu y=Cxy = Cxwhere xx is the state vector, uu is the input vector, and yy is the output vector.

STEP 12

In our case, u=[TinF]u = \begin{bmatrix} T_{in} \\ F \end{bmatrix} and y=vy = v.

STEP 13

From the given equations and relationships, we can derive the matrices AA, BB, and CC: A=[c1J00c2m],B=[1JrJ01m],C=[01]A = \begin{bmatrix} -\frac{c_1}{J} & 0 \\ 0 & -\frac{c_2}{m} \end{bmatrix}, \quad B = \begin{bmatrix} \frac{1}{J} & -\frac{r}{J} \\ 0 & \frac{1}{m} \end{bmatrix}, \quad C = \begin{bmatrix} 0 & 1 \end{bmatrix}

STEP 14

The relationship between input torque and velocity is: Tin=(Jr+mr)dvdt+(c1r+rc2)vT_{in} = \left( \frac{J}{r} + mr \right) \cdot \frac{dv}{dt} + \left( \frac{c_1}{r} + rc_2 \right) \cdot v The state-space representation is: dxdt=[c1J00c2m]x+[1JrJ01m]u\frac{dx}{dt} = \begin{bmatrix} -\frac{c_1}{J} & 0 \\ 0 & -\frac{c_2}{m} \end{bmatrix}x + \begin{bmatrix} \frac{1}{J} & -\frac{r}{J} \\ 0 & \frac{1}{m} \end{bmatrix}u y=[01]xy = \begin{bmatrix} 0 & 1 \end{bmatrix}x

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