Optimal projection equations

The reduced-order LQG control problem is almost identical to the conventional full-order LQG control problem. Let ${\displaystyle {\hat {\mathbf {x} }}_{r}(t)}$ represent the state of the reduced-order LQG controller. Then the only difference is that the state dimension ${\displaystyle n_{r}=dim({\hat {\mathbf {x} }}_{r}(t))}$ of the LQG controller is a-priori fixed to be smaller than ${\displaystyle n=dim({\mathbf {x} }(t))}$, the state dimension of the controlled system.

The reduced-order LQG controller is represented by the following equations:

${\displaystyle {\dot {\hat {\mathbf {x} }}}_{r}(t)=A_{r}(t){\hat {\mathbf {x} }}_{r}(t)+B_{r}(t){\mathbf {u} }(t)+K_{r}(t)\left({\mathbf {y} }(t)-C_{r}(t){\hat {\mathbf {x} }}_{r}(t)\right),{\hat {\mathbf {x} }}_{r}(0)={\mathbf {x} }_{r}(0),}$

${\displaystyle {\mathbf {u} }(t)=-L_{r}(t){\hat {\mathbf {x} }}_{r}(t).}$

These equations are deliberately stated in a format that equals that of the conventional full-order LQG controller. For the reduced-order LQG control problem it is convenient to rewrite them as

${\displaystyle {\dot {\hat {\mathbf {x} }}}_{r}(t)=F_{r}(t){\hat {\mathbf {x} }}_{r}(t)+K_{r}(t){\mathbf {y} }(t),{\hat {\mathbf {x} }}_{r}(0)={\mathbf {x} }_{r}(0),}$

${\displaystyle {\mathbf {u} }(t)=-L_{r}(t){\hat {\mathbf {x} }}_{r}(t),}$

where

${\displaystyle F_{r}(t)=A_{r}(t)-B_{r}(t)L_{r}(t)-K_{r}(t)C_{r}(t).}$

The matrices ${\displaystyle F_{r}(t),K_{r}(t),L_{r}(t)}$ and ${\displaystyle {\mathbf {x} }_{r}(0)}$ of the reduced-order LQG controller are determined by the so-called optimal projection equations (OPE).[3]

The square optimal projection matrix ${\displaystyle \tau (t)}$ with dimension ${\displaystyle n}$ is central to the OPE. The rank of this matrix is almost everywhere equal to ${\displaystyle n_{r}.}$ The associated projection is an oblique projection: ${\displaystyle \tau ^{2}(t)=\tau (t).}$ The OPE constitute four matrix differential equations. The first two equations listed below are generalizations of the matrix Riccati differential equations associated to the conventional full-order LQG controller. In these equations ${\displaystyle \tau _{\perp }(t)}$ denotes ${\displaystyle I_{n}-\tau (t)}$ where ${\displaystyle I_{n}}$ is the identity matrix of dimension ${\displaystyle n}$.

${\displaystyle {\begin{aligned}{\dot {P}}(t)={}&A(t)P(t)+P(t)A'(t)-P(t)C'(t)W^{-1}(t)C(t)P(t)+V(t)\\[6pt]&{}+\tau _{\perp }(t)P(t)C'(t)W^{-1}(t)C(t)P(t)\tau '_{\perp }(t),\\[6pt]P(0)={}&E\left({\mathbf {x} }(0){\mathbf {x} }'(0)\right),\\[6pt]&{}-{\dot {S}}(t)=A'(t)S(t)+S(t)A(t)-S(t)B(t)R^{-1}(t)B'(t)S(t)+Q(t)\\[6pt]&{}+\tau '_{\perp }(t)S(t)B(t)R^{-1}(t)B'(t)S(t)\tau _{\perp }(t),\end{aligned}}}$

${\displaystyle S(T)=F.}$

If the dimension of the LQG controller is not reduced, that is if ${\displaystyle n=n_{r}}$, then ${\displaystyle \tau (t)=I_{n},\tau _{\perp }(t)=0}$ and the two equations above become the uncoupled matrix Riccati differential equations associated to the conventional full-order LQG controller. If ${\displaystyle n_{r}<n}$ the two equations are coupled by the oblique projection ${\displaystyle \tau (t).}$ This reveals why the reduced-order LQG problem is not separable. The oblique projection ${\displaystyle \tau (t)}$ is determined from two additional matrix differential equations which involve rank conditions. Together with the previous two matrix differential equations these are the OPE. To state the additional two matrix differential equations it is convenient to introduce the following two matrices:

${\displaystyle \Psi _{1}(t)=(A(t)-B(t)R^{-1}(t)B'(t)S(t)){\hat {P}}(t)+{\hat {P}}(t)(A(t)-B(t)R^{-1}(t)B'(t)S(t))'}$

${\displaystyle {}+P(t)C'(t)W^{-1}(t)C(t)P(t),}$

${\displaystyle \Psi _{2}(t)=(A(t)-P(t)C'(t)W^{-1}(t)C(t))'{\hat {S}}(t)+{\hat {S}}(t)(A(t)-P(t)C'(t)W^{-1}(t)C(t))}$

${\displaystyle {}+S(t)B(t)R^{-1}(t)B'(t)S(t).}$

Then the two additional matrix differential equations that complete the OPE are as follows:

${\displaystyle {\dot {\hat {P}}}(t)=1/2\left(\tau (t)\Psi _{1}(t)+\Psi _{1}(t)\tau '(t)\right),{\hat {P}}(0)=E({\mathbf {x} }(0))E({\mathbf {x} }(0))',\operatorname {rank} ({\hat {P}}(t))=n_{r}}$ almost everywhere,

${\displaystyle -{\dot {\hat {S}}}(t)=1/2\left(\tau '(t)\Psi _{2}(t)+\Psi _{2}(t)\tau (t)\right),{\hat {S}}(T)=0,\operatorname {rank} ({\hat {S}}(t))=n_{r}}$ almost everywhere,

with

${\displaystyle \tau (t)={\hat {P}}(t){\hat {S}}(t)\left({\hat {P}}(t){\hat {S}}(t)\right)^{*}.}$

Here * denotes the group generalized inverse or Drazin inverse that is unique and given by

${\displaystyle A^{*}=A(A^{3})^{+}A.}$

where + denotes the Moore–Penrose pseudoinverse.

The matrices ${\displaystyle P(t),S(t),{\hat {P}}(t),{\hat {S}}(t)}$ must all be nonnegative symmetric. Then they constitute a solution of the OPE that determines the reduced-order LQG controller matrices ${\displaystyle F_{r}(t),K_{r}(t),L_{r}(t)}$ and ${\displaystyle {\mathbf {x} }_{r}(0)}$:

${\displaystyle F_{r}(t)=H(t)\left(A(t)-P(t)C'(t)W^{-1}(t)C(t)-B(t)R^{-1}(t)B'(t)S(t)\right)G(t)+{\dot {H}}(t)G'(t),}$

${\displaystyle K_{r}(t)=H(t)P(t)C'(t)W^{-1}(t),}$

${\displaystyle L_{r}(t)=R^{-1}(t)B'(t)S(t)G'(t),}$

${\displaystyle {\mathbf {x} }_{r}(0)=H(0)E({\mathbf {x} }(0)).}$

In the equations above the matrices ${\displaystyle G(t),H(t)}$ are two matrices with the following properties:

${\displaystyle G'(t)H(t)=\tau (t),G(t)H'(t)=I_{n_{r}}}$ almost everywhere.

They can be obtained from a projective factorization of ${\displaystyle {\hat {P}}(t){\hat {S}}(t)}$.[4]

The OPE can be stated in many different ways that are all equivalent. To identify the equivalent representations the following identities are especially useful:

${\displaystyle \tau (t){\hat {P}}(t)={\hat {P}}(t)\tau '(t)={\hat {P}}(t),\tau '(t){\hat {S}}(t)={\hat {S}}(t)\tau (t)={\hat {S}}(t)}$

Using these identities one may for instance rewrite the first two of the optimal projection equations as follows:

${\displaystyle {\dot {P}}(t)=A(t)P(t)+P(t)A'(t)-P(t)C'(t)W^{-1}(t)C(t)P(t)+V(t)+\tau _{\perp }(t)\Psi _{1}(t)\tau '_{\perp }(t),}$

${\displaystyle P(0)=E\left({\mathbf {x} }(0){\mathbf {x} }'(0)\right),}$

${\displaystyle -{\dot {S}}(t)=A'(t)S(t)+S(t)A(t)-S(t)B(t)R^{-1}(t)B'(t)S(t)+Q(t)+\tau '_{\perp }\Psi _{2}(t)\tau _{\perp }(t),}$

${\displaystyle S(T)=F.}$

This representation is both relatively simple and suitable for numerical computations.

If all the matrices in the reduced-order LQG problem formulation are time-invariant and if the horizon ${\displaystyle T}$ tends to infinity, the optimal reduced-order LQG controller becomes time-invariant and so do the OPE.[1] In that case the derivatives on the left hand side of the OPE are zero.

Similar to the continuous-time case, in the discrete-time case the difference with the conventional discrete-time full-order LQG problem is the a-priori fixed reduced-order ${\displaystyle n_{r}<n}$ of the LQG controller state dimension. As in continuous-time, to state the discrete-time OPE it is convenient to introduce the following two matrices:

${\displaystyle \Psi _{i}^{1}=\left(A_{i}-B_{i}(B'_{i}S_{i+1}B_{i}+R_{i})^{-1}B'_{i}S_{i+1}A_{i})\right){\hat {P}}_{i}\left(A_{i}-B_{i}(B'_{i}S_{i+1}B_{i}+R_{i})^{-1}B'_{i}S_{i+1}A_{i})\right)'}$

${\displaystyle {}+A_{i}P_{i}C'_{i}(C_{i}P_{i}C'_{i}+W_{i})^{-1}C_{i}P_{i}A'_{i}}$

${\displaystyle \Psi _{i+1}^{2}=\left(A_{i}-A_{i}P_{i}C'_{i}(C_{i}P_{i}C'_{i}+W_{i})^{-1}C_{i}\right)'{\hat {S}}_{i+1}\left(A_{i}-A_{i}P_{i}C'_{i}(C_{i}P_{i}C'_{i}+W_{i})^{-1}C_{i}\right)}$

${\displaystyle {}+A'_{i}S_{i+1}B_{i}(B'_{i}S_{i+1}B_{i}+R_{i})^{-1}B'_{i}S_{i+1}A_{i}}$

Then the discrete-time OPE is

${\displaystyle P_{i+1}=A_{i}\left(P_{i}-P_{i}C'_{i}\left(C_{i}P_{i}C'_{i}+W_{i}\right)^{-1}C_{i}P_{i}\right)A'_{i}+V_{i}+\tau _{\perp i+1}\Psi _{i}^{1}\tau '_{\perp i+1},P_{0}=E\left({\mathbf {x} }_{0}{\mathbf {x'} }_{0}\right)}$.

${\displaystyle S_{i}=A'_{i}\left(S_{i+1}-S_{i+1}B_{i}\left(B'_{i}S_{i+1}B_{i}+R_{i}\right)^{-1}B'_{i}S_{i+1}\right)A_{i}+Q_{i}+\tau '_{\perp i}\Psi _{i+1}^{2}\tau _{\perp i},S_{N}=F}$.

${\displaystyle {\hat {P}}_{i+1}=1/2(\tau _{i+1}\Psi _{i}^{1}+\Psi _{i}^{1}\tau '_{i+1}),{\hat {P}}_{0}=E({\mathbf {x} }(0))E({\mathbf {x} }(0))',\operatorname {rank} ({\hat {P}}_{i})=n_{r}}$ almost everywhere,

${\displaystyle {\hat {S}}_{i}=1/2(\tau '_{i}\Psi _{i+1}^{2}+\Psi _{i+1}^{2}\tau _{i}),{\hat {S}}_{N}=0,\operatorname {rank} ({\hat {S}}_{i})=n_{r}}$ almost everywhere.

The oblique projection matrix is given by

${\displaystyle \tau _{i}={\hat {P}}_{i}{\hat {S}}_{i}\left({\hat {P}}_{i}{\hat {S}}_{i}\right)^{*}.}$

The nonnegative symmetric matrices ${\displaystyle P_{i},S_{i},{\hat {P}}_{i},{\hat {S}}_{i}}$ that solve the discrete-time OPE determine the reduced-order LQG controller matrices ${\displaystyle F_{i}^{r},K_{i}^{r},L_{i}^{r}}$ and ${\displaystyle {\mathbf {x} }_{0}^{r}}$:

${\displaystyle F_{i}^{r}=H_{i+1}\left(A_{i}-P_{i}C'_{i}\left(C_{i}P_{i}C'_{i}+W_{i}\right)^{-1}C_{i}-B_{i}\left(B'_{i}S_{i+1}B_{i}+R_{i}\right)^{-1}B'_{i}S_{i+1}\right)G'_{i},}$

${\displaystyle K_{i}^{r}=H_{i+1}P_{i}C'_{i}\left(C_{i}P_{i}C'_{i}+W_{i}\right)^{-1},}$

${\displaystyle L_{i}^{r}=\left(B'_{i}S_{i+1}B_{i}+R_{i}\right)^{-1}B'_{i}S_{i+1}G'_{i},}$

${\displaystyle {\mathbf {x} }_{0}^{r}=H_{0}E({\mathbf {x} }_{0}).}$

In the equations above the matrices ${\displaystyle G_{i},H_{i}}$ are two matrices with the following properties:

${\displaystyle G'_{i}H_{i}=\tau _{i},G_{i}H'_{i}=I_{n_{r}}}$ almost everywhere.

They can be obtained from a projective factorization of ${\displaystyle {\hat {P}}_{i}{\hat {S}}_{i}}$.[4] To identify equivalent representations of the discrete-time OPE the following identities are especially useful:

${\displaystyle \tau _{i}{\hat {P}}_{i}={\hat {P}}_{i}\tau '_{i}={\hat {P}}_{i},\tau '_{i}{\hat {S}}_{i}={\hat {S}}_{i}\tau _{i}={\hat {S}}_{i}}$

As in the continuous-time case if all the matrices in the problem formulation are time-invariant and if the horizon ${\displaystyle N}$ tends to infinity the reduced-order LQG controller becomes time-invariant. Then the discrete-time OPE converge to a steady state solution that determines the time-invariant reduced-order LQG controller.[2]

The discrete-time OPE apply also to discrete-time systems with variable state, input and output dimensions (discrete-time systems with time-varying dimensions).[6] Such systems arise in the case of digital controller design if the sampling occurs asynchronously.