Rewrite second order non-homogeneous differential equation as a first order systemFurther explanation needed for this first order system of linear equations which is as follows:Differential equation of a mass on a springSolving a system of equation modul0 5Stability for Nonlinear SystemConverting second order system into first order system (ODE)Calculate equilibrium points of a 2nd order systemFinding a matrix for a system of differential equationsSolve differential equation by using polar coordinatesConvert equation system in to one ODESolving system of first order differential equations using eigenvalue /eigenvector and matrix exponential approaches

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Rewrite second order non-homogeneous differential equation as a first order system


Further explanation needed for this first order system of linear equations which is as follows:Differential equation of a mass on a springSolving a system of equation modul0 5Stability for Nonlinear SystemConverting second order system into first order system (ODE)Calculate equilibrium points of a 2nd order systemFinding a matrix for a system of differential equationsSolve differential equation by using polar coordinatesConvert equation system in to one ODESolving system of first order differential equations using eigenvalue /eigenvector and matrix exponential approaches













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$begingroup$


Question: I believe I am correct up until $y(t) = Cx(t)$. I was told I did it incorrectly, but I cannot figure out how to grab the position of the antenna using $y(t) = Cx(t)$. Does it look correct, if not, how can I go about finding $y(t)$? I am stumped.




We want to design and simulate a full state feedback LQR control law for a
rotating antenna. The motion of the antenna can be described by the linear second order non-homogeneous differential equation given by $$Iθ''(t) + cθ'(t) = τ (t)$$ with initial conditions: $$θ(0) = θ_0$$ $$θ'(0) = θ_1$$ where $I$ is the effective moment of inertia of all the rotating parts including the antenna,
$c ≥ 0$ is the coefficient of viscous (i.e. air; the antenna is in low earth atmosphere, not the vacuum of space) friction, $τ (t)$ is the torque applied by the motor that effects the rotation at time $t ≥ 0$, and $θ(t)$ is the angular position of the antenna at time $t ≥ 0$.



(The basis for the model is simply Newton’s second law, $F = ma$, in the context of rotary motion, i.e. torque equals the moment of inertia times the angular acceleration. The friction term is modeled as a torque that is proportional to the velocity so that it is in the direction opposite to the motion of the antenna.)



The motor torque at time $t ≥ 0$ is assumed to be proportional to $u(t)$, the input voltage to the motor, with constant of proportionality $b > 0$.



In your calculations below use the following values: $alpha = fraccI=4.6s^-1,$ $λ = fracbI = 0.787 fracradVs2 $, and $I = 10kgm^2.$



The output variable is the angular position of the antenna.



Rewrite the model as a first order system of the form $$x'(t) = Ax(t) + Bu(t)$$ $$y(t) = Cx(t)$$ $$x(0) = x_0.$$




ATTEMPT:
$$Itheta''(t) + ctheta'(t) + 0theta(t)= tau(t)$$
$$theta''(t) = frac1Itau(t)-fraccItheta'(t)-0theta(t)$$
$$x_1=theta(t)$$
$$x_2 =theta'(t)$$
$$x_1'(t) = theta'(t)$$
$$x_2'(t) = theta''(t)=fracbIu(t)-fraccItheta'(t)-0theta(t)$$
$$x_1(0) = theta(0) = theta_0$$
$$x_2(0) = theta'(t) = theta_1$$
$$x_1'(t) = 0x_1(t)+1x_2(t)+0$$
$$x_2'(t) = 0x_1(t) -fraccIx_2(t)+fracbIu(t)$$
$$x'(t)=beginpmatrixx_1'\ x_2' endpmatrix=beginpmatrix0 & 1\ 0 & frac-cIendpmatrixx(t)+beginpmatrix0\ fracbIendpmatrixu(t)$$
$$y(t)=beginpmatrix1\ 0endpmatrixx(t)$$
$$x(0)=beginpmatrixtheta_0\ theta_1endpmatrix$$










share|cite|improve this question











$endgroup$
















    1












    $begingroup$


    Question: I believe I am correct up until $y(t) = Cx(t)$. I was told I did it incorrectly, but I cannot figure out how to grab the position of the antenna using $y(t) = Cx(t)$. Does it look correct, if not, how can I go about finding $y(t)$? I am stumped.




    We want to design and simulate a full state feedback LQR control law for a
    rotating antenna. The motion of the antenna can be described by the linear second order non-homogeneous differential equation given by $$Iθ''(t) + cθ'(t) = τ (t)$$ with initial conditions: $$θ(0) = θ_0$$ $$θ'(0) = θ_1$$ where $I$ is the effective moment of inertia of all the rotating parts including the antenna,
    $c ≥ 0$ is the coefficient of viscous (i.e. air; the antenna is in low earth atmosphere, not the vacuum of space) friction, $τ (t)$ is the torque applied by the motor that effects the rotation at time $t ≥ 0$, and $θ(t)$ is the angular position of the antenna at time $t ≥ 0$.



    (The basis for the model is simply Newton’s second law, $F = ma$, in the context of rotary motion, i.e. torque equals the moment of inertia times the angular acceleration. The friction term is modeled as a torque that is proportional to the velocity so that it is in the direction opposite to the motion of the antenna.)



    The motor torque at time $t ≥ 0$ is assumed to be proportional to $u(t)$, the input voltage to the motor, with constant of proportionality $b > 0$.



    In your calculations below use the following values: $alpha = fraccI=4.6s^-1,$ $λ = fracbI = 0.787 fracradVs2 $, and $I = 10kgm^2.$



    The output variable is the angular position of the antenna.



    Rewrite the model as a first order system of the form $$x'(t) = Ax(t) + Bu(t)$$ $$y(t) = Cx(t)$$ $$x(0) = x_0.$$




    ATTEMPT:
    $$Itheta''(t) + ctheta'(t) + 0theta(t)= tau(t)$$
    $$theta''(t) = frac1Itau(t)-fraccItheta'(t)-0theta(t)$$
    $$x_1=theta(t)$$
    $$x_2 =theta'(t)$$
    $$x_1'(t) = theta'(t)$$
    $$x_2'(t) = theta''(t)=fracbIu(t)-fraccItheta'(t)-0theta(t)$$
    $$x_1(0) = theta(0) = theta_0$$
    $$x_2(0) = theta'(t) = theta_1$$
    $$x_1'(t) = 0x_1(t)+1x_2(t)+0$$
    $$x_2'(t) = 0x_1(t) -fraccIx_2(t)+fracbIu(t)$$
    $$x'(t)=beginpmatrixx_1'\ x_2' endpmatrix=beginpmatrix0 & 1\ 0 & frac-cIendpmatrixx(t)+beginpmatrix0\ fracbIendpmatrixu(t)$$
    $$y(t)=beginpmatrix1\ 0endpmatrixx(t)$$
    $$x(0)=beginpmatrixtheta_0\ theta_1endpmatrix$$










    share|cite|improve this question











    $endgroup$














      1












      1








      1





      $begingroup$


      Question: I believe I am correct up until $y(t) = Cx(t)$. I was told I did it incorrectly, but I cannot figure out how to grab the position of the antenna using $y(t) = Cx(t)$. Does it look correct, if not, how can I go about finding $y(t)$? I am stumped.




      We want to design and simulate a full state feedback LQR control law for a
      rotating antenna. The motion of the antenna can be described by the linear second order non-homogeneous differential equation given by $$Iθ''(t) + cθ'(t) = τ (t)$$ with initial conditions: $$θ(0) = θ_0$$ $$θ'(0) = θ_1$$ where $I$ is the effective moment of inertia of all the rotating parts including the antenna,
      $c ≥ 0$ is the coefficient of viscous (i.e. air; the antenna is in low earth atmosphere, not the vacuum of space) friction, $τ (t)$ is the torque applied by the motor that effects the rotation at time $t ≥ 0$, and $θ(t)$ is the angular position of the antenna at time $t ≥ 0$.



      (The basis for the model is simply Newton’s second law, $F = ma$, in the context of rotary motion, i.e. torque equals the moment of inertia times the angular acceleration. The friction term is modeled as a torque that is proportional to the velocity so that it is in the direction opposite to the motion of the antenna.)



      The motor torque at time $t ≥ 0$ is assumed to be proportional to $u(t)$, the input voltage to the motor, with constant of proportionality $b > 0$.



      In your calculations below use the following values: $alpha = fraccI=4.6s^-1,$ $λ = fracbI = 0.787 fracradVs2 $, and $I = 10kgm^2.$



      The output variable is the angular position of the antenna.



      Rewrite the model as a first order system of the form $$x'(t) = Ax(t) + Bu(t)$$ $$y(t) = Cx(t)$$ $$x(0) = x_0.$$




      ATTEMPT:
      $$Itheta''(t) + ctheta'(t) + 0theta(t)= tau(t)$$
      $$theta''(t) = frac1Itau(t)-fraccItheta'(t)-0theta(t)$$
      $$x_1=theta(t)$$
      $$x_2 =theta'(t)$$
      $$x_1'(t) = theta'(t)$$
      $$x_2'(t) = theta''(t)=fracbIu(t)-fraccItheta'(t)-0theta(t)$$
      $$x_1(0) = theta(0) = theta_0$$
      $$x_2(0) = theta'(t) = theta_1$$
      $$x_1'(t) = 0x_1(t)+1x_2(t)+0$$
      $$x_2'(t) = 0x_1(t) -fraccIx_2(t)+fracbIu(t)$$
      $$x'(t)=beginpmatrixx_1'\ x_2' endpmatrix=beginpmatrix0 & 1\ 0 & frac-cIendpmatrixx(t)+beginpmatrix0\ fracbIendpmatrixu(t)$$
      $$y(t)=beginpmatrix1\ 0endpmatrixx(t)$$
      $$x(0)=beginpmatrixtheta_0\ theta_1endpmatrix$$










      share|cite|improve this question











      $endgroup$




      Question: I believe I am correct up until $y(t) = Cx(t)$. I was told I did it incorrectly, but I cannot figure out how to grab the position of the antenna using $y(t) = Cx(t)$. Does it look correct, if not, how can I go about finding $y(t)$? I am stumped.




      We want to design and simulate a full state feedback LQR control law for a
      rotating antenna. The motion of the antenna can be described by the linear second order non-homogeneous differential equation given by $$Iθ''(t) + cθ'(t) = τ (t)$$ with initial conditions: $$θ(0) = θ_0$$ $$θ'(0) = θ_1$$ where $I$ is the effective moment of inertia of all the rotating parts including the antenna,
      $c ≥ 0$ is the coefficient of viscous (i.e. air; the antenna is in low earth atmosphere, not the vacuum of space) friction, $τ (t)$ is the torque applied by the motor that effects the rotation at time $t ≥ 0$, and $θ(t)$ is the angular position of the antenna at time $t ≥ 0$.



      (The basis for the model is simply Newton’s second law, $F = ma$, in the context of rotary motion, i.e. torque equals the moment of inertia times the angular acceleration. The friction term is modeled as a torque that is proportional to the velocity so that it is in the direction opposite to the motion of the antenna.)



      The motor torque at time $t ≥ 0$ is assumed to be proportional to $u(t)$, the input voltage to the motor, with constant of proportionality $b > 0$.



      In your calculations below use the following values: $alpha = fraccI=4.6s^-1,$ $λ = fracbI = 0.787 fracradVs2 $, and $I = 10kgm^2.$



      The output variable is the angular position of the antenna.



      Rewrite the model as a first order system of the form $$x'(t) = Ax(t) + Bu(t)$$ $$y(t) = Cx(t)$$ $$x(0) = x_0.$$




      ATTEMPT:
      $$Itheta''(t) + ctheta'(t) + 0theta(t)= tau(t)$$
      $$theta''(t) = frac1Itau(t)-fraccItheta'(t)-0theta(t)$$
      $$x_1=theta(t)$$
      $$x_2 =theta'(t)$$
      $$x_1'(t) = theta'(t)$$
      $$x_2'(t) = theta''(t)=fracbIu(t)-fraccItheta'(t)-0theta(t)$$
      $$x_1(0) = theta(0) = theta_0$$
      $$x_2(0) = theta'(t) = theta_1$$
      $$x_1'(t) = 0x_1(t)+1x_2(t)+0$$
      $$x_2'(t) = 0x_1(t) -fraccIx_2(t)+fracbIu(t)$$
      $$x'(t)=beginpmatrixx_1'\ x_2' endpmatrix=beginpmatrix0 & 1\ 0 & frac-cIendpmatrixx(t)+beginpmatrix0\ fracbIendpmatrixu(t)$$
      $$y(t)=beginpmatrix1\ 0endpmatrixx(t)$$
      $$x(0)=beginpmatrixtheta_0\ theta_1endpmatrix$$







      matrices ordinary-differential-equations






      share|cite|improve this question















      share|cite|improve this question













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      edited Mar 21 at 13:00









      Cameron Buie

      86.3k773161




      86.3k773161










      asked Mar 21 at 8:27









      PattyWatty27PattyWatty27

      435




      435




















          1 Answer
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          $begingroup$

          You came incredibly close!



          It seems that you want $y(t)=theta(t)=x_1(t).$ Unfortunately, we can't multiply two $2times 1$ matrices together. In general, if $M$ and $N$ are non-scalar matrices (that is, neither has only one row and one column), say with $M$ being $ktimes m$ and $N$ being $ntimes p,$ we will have $MN$ defined only if $m=n,$ in which case $MN$ will be a $ktimes p$ matrix.



          Instead, you want $$y(t)=beginpmatrix1 & 0endpmatrixx(t).$$ By multiplying any $1times 2$ matrix and a $2times 1$ matrix together, we obtain a $1times 1$ matrix--a scalar--as desired.






          share|cite|improve this answer











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            active

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            $begingroup$

            You came incredibly close!



            It seems that you want $y(t)=theta(t)=x_1(t).$ Unfortunately, we can't multiply two $2times 1$ matrices together. In general, if $M$ and $N$ are non-scalar matrices (that is, neither has only one row and one column), say with $M$ being $ktimes m$ and $N$ being $ntimes p,$ we will have $MN$ defined only if $m=n,$ in which case $MN$ will be a $ktimes p$ matrix.



            Instead, you want $$y(t)=beginpmatrix1 & 0endpmatrixx(t).$$ By multiplying any $1times 2$ matrix and a $2times 1$ matrix together, we obtain a $1times 1$ matrix--a scalar--as desired.






            share|cite|improve this answer











            $endgroup$

















              1












              $begingroup$

              You came incredibly close!



              It seems that you want $y(t)=theta(t)=x_1(t).$ Unfortunately, we can't multiply two $2times 1$ matrices together. In general, if $M$ and $N$ are non-scalar matrices (that is, neither has only one row and one column), say with $M$ being $ktimes m$ and $N$ being $ntimes p,$ we will have $MN$ defined only if $m=n,$ in which case $MN$ will be a $ktimes p$ matrix.



              Instead, you want $$y(t)=beginpmatrix1 & 0endpmatrixx(t).$$ By multiplying any $1times 2$ matrix and a $2times 1$ matrix together, we obtain a $1times 1$ matrix--a scalar--as desired.






              share|cite|improve this answer











              $endgroup$















                1












                1








                1





                $begingroup$

                You came incredibly close!



                It seems that you want $y(t)=theta(t)=x_1(t).$ Unfortunately, we can't multiply two $2times 1$ matrices together. In general, if $M$ and $N$ are non-scalar matrices (that is, neither has only one row and one column), say with $M$ being $ktimes m$ and $N$ being $ntimes p,$ we will have $MN$ defined only if $m=n,$ in which case $MN$ will be a $ktimes p$ matrix.



                Instead, you want $$y(t)=beginpmatrix1 & 0endpmatrixx(t).$$ By multiplying any $1times 2$ matrix and a $2times 1$ matrix together, we obtain a $1times 1$ matrix--a scalar--as desired.






                share|cite|improve this answer











                $endgroup$



                You came incredibly close!



                It seems that you want $y(t)=theta(t)=x_1(t).$ Unfortunately, we can't multiply two $2times 1$ matrices together. In general, if $M$ and $N$ are non-scalar matrices (that is, neither has only one row and one column), say with $M$ being $ktimes m$ and $N$ being $ntimes p,$ we will have $MN$ defined only if $m=n,$ in which case $MN$ will be a $ktimes p$ matrix.



                Instead, you want $$y(t)=beginpmatrix1 & 0endpmatrixx(t).$$ By multiplying any $1times 2$ matrix and a $2times 1$ matrix together, we obtain a $1times 1$ matrix--a scalar--as desired.







                share|cite|improve this answer














                share|cite|improve this answer



                share|cite|improve this answer








                edited Mar 21 at 13:10

























                answered Mar 21 at 12:57









                Cameron BuieCameron Buie

                86.3k773161




                86.3k773161



























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