Reduced state estimation with multisensor fusion and out-of-sequence measurements
First Claim
1. A method for recursively estimating the state of a system having multidimensional parameters λ
- in addition to state variables x(k) at time tk for k=1,2,3, . . . , which parameters λ
are unknown, arbitrarily time-varying, but bounded, and driven by the input function u(x(k),λ
) and governed by the state equation
x(k+1)=Φ
x(k)+Γ
u(x(k),λ
)where Φ
,Γ
are system matrices dependent on the discrete time interval T=tk+1−
tk;
said method comprising the following steps;
measuring aspects of the state of the system to produce initial measurements;
initializing state estimates {circumflex over (x)}(k0|k0) and the matrices M(k0|k0), D(k0|k0) using a priori information and the initial measurements,wherevector {circumflex over (x)}(t|k) is defined as the estimate of the state of the system at time t after processing the measurements z(i) for 1≦
i≦
k;
vector {circumflex over (x)}(tj|k) is denoted as {circumflex over (x)}(j|k) when the time t=tj is the time of the jth measurement for j=1,2,3, . . . ;
matrix M(t|k) is defined as the covariance of the state estimation errors at time t due only to the errors in the measurements z(i) for 1≦
i≦
k and a priori initial information that is independent of the parameter uncertainty;
matrix M(tj|k) is denoted as M(j|k), when the time t=tj is the time of the jth measurement for j=1,2,3, . . . ;
matrix D(t|k) is defined as the matrix of bias coefficients, which linearly relates state estimation errors to the parameter errors, at time t (after processing k=0,1,2, . . . measurements);
matrix D(tj|k) is denoted as D(j|k), when the time t=tj is the time of the jth measurement for j=1,2,3, . . . ;
determining the time tk+1 of a new measurement and the time t when the filter was last updated;
using the update interval T=tk+1−
t, determine the system transition matrices Φ and
Γ
;
determining the mean value {overscore (λ
)} of unknown but bounded parameters λ
, and the input vector u({circumflex over (x)}(t|k),{overscore (λ
)});
measuring aspects of the state of the system governed by the measurement equation
z(k)=Hx(k)+n(k)
where n(k) is the measurement noise with covariance N and measurement matrix H at time tk for k=1,2,3, . . . ;
determining if the measurement is time-late by testing T<
0;
(a) if the measurement is time-late determining F,G as follows generating a parameter matrix Λ
, representing physical bounds on the parameters λ
that are not state variables of the system;
extrapolating said state estimates {circumflex over (x)}(t|k) and matrices M(t|k), D(t|k), to {circumflex over (x)}(k+1|k), M(k+1|k), D(k+1|k), and calculating S(k+1|k) as in
{circumflex over (x)}(k+1|k)=Φ
{circumflex over (x)}(t|k)+Γ
u({circumflex over (x)}(t|k),{overscore (λ
)})
M(k+1|k)=FM(t|k)F′
D(k+1|k)=FD(t|k)+G
S(k+1|k)=M(k+1|k)+D(k+1|k)Λ
D(k+1|k)′
determining covariance of the residual Q as in
Q=HS(k+1|k)H′
+N determining the filter gain matrix K as in
K=[M(t|k)F′
+D(t|k)Λ
D(k+1|k)′
]H′
Q−
1 determining the matrix L as in
L=I−
KHF
where I is the identity matrix;
updating the state estimate {circumflex over (x)}(t|k) as
{circumflex over (x)}(t|k+1)={circumflex over (x)}(t|k)+K[z(k+1)−
H{circumflex over (x)}(k+1|k)]updating the matrices M(t|k) and D(t|k) as
M(t|k+1)=LM(t|k)L′
+KNK′
D(t|k+1)=D(t|k)−
KHD(k+1|k)
respectively, and generating the total mean square error S(t|k+1) as in
S(t|k+1)=M(t|k+1)+D(t|k+1)Λ
D(t|k+1)′
(b) and if the measurement is not time-late determining F,G using and, generating a parameter matrix Λ
, representing physical bounds on those parameters that are not state variables of the system;
extrapolating said state estimates {circumflex over (x)}(k|k) and matrices M(k|k), D(k|k), S(k|k) to {circumflex over (x)}(k+1|k), M(k+1|k), D(k+1|k), and S(k+1|k) as in
{circumflex over (x)}(k+1|k)=Φ
{circumflex over (x)}(k|k)+Γ
u({circumflex over (x)}(k|k),{overscore (λ
)})
M(k+1|k)=FM(k|k)F′
D(k+1|k)=FD(k|k)+G
S(k+1|k)=M(k+1|k)+D(k+1|k)Λ
D(k+1|k)′
determining covariance of the residual Q as in
Q=HS(k+1|k)H′
+N determining the filter gain matrix K as in
K=S(k+1|k)H′
Q−
1 determining the matrix L as in
L=I−
KH
where I is the identity matrix;
updating the state estimate {circumflex over (x)}(k+1|k) as
{circumflex over (x)}(k+1|k+1)={circumflex over (x)}(k+1|k)+K[z(k+1)−
H{circumflex over (x)}(k+1|k)]updating the matrices M(k+1|k) and D(k+1|k) as
M(k+1|k+1)=LM(k+1|k)L′
+KNK′
and,
D(k+1|k+1)=LD(k+1|k)respectively, and generating the total mean square error S(k+1|k+1) as
S(k+1|k+1)=M(k+1|k+1)+D(k+1|k+1)Λ
D(k+1|k+1)′
after
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Abstract
This invention relates to state estimation after processing measurements with time delays from multiple sensors of systems characterized by state variables and by multidimensional parameters, for which the latter are unknown and may vary arbitrarily in time within known physical bounds. If a measurement is time-late, apply the measurement to an out-of-sequence filter that uses a mean square optimization criterion that accounts for measurement errors and said bounding values, as well as the delay time, to optimally produce estimates of the true states of the system. If the measurement is not time-late, apply the measurements to an in-sequence filter that uses a mean square optimization criterion that accounts for measurement errors and said bounding values, to produce estimates of the true states of the system. The estimates are applied to one of (a) making a decision relating to the system, (b) operating a control system, and (c) controlling a process.
27 Citations
2 Claims
-
1. A method for recursively estimating the state of a system having multidimensional parameters λ
- in addition to state variables x(k) at time tk for k=1,2,3, . . . , which parameters λ
are unknown, arbitrarily time-varying, but bounded, and driven by the input function u(x(k),λ
) and governed by the state equation
x(k+1)=Φ
x(k)+Γ
u(x(k),λ
)where Φ
,Γ
are system matrices dependent on the discrete time interval T=tk+1−
tk;
said method comprising the following steps;measuring aspects of the state of the system to produce initial measurements; initializing state estimates {circumflex over (x)}(k0|k0) and the matrices M(k0|k0), D(k0|k0) using a priori information and the initial measurements, where vector {circumflex over (x)}(t|k) is defined as the estimate of the state of the system at time t after processing the measurements z(i) for 1≦
i≦
k;vector {circumflex over (x)}(tj|k) is denoted as {circumflex over (x)}(j|k) when the time t=tj is the time of the jth measurement for j=1,2,3, . . . ; matrix M(t|k) is defined as the covariance of the state estimation errors at time t due only to the errors in the measurements z(i) for 1≦
i≦
k and a priori initial information that is independent of the parameter uncertainty;matrix M(tj|k) is denoted as M(j|k), when the time t=tj is the time of the jth measurement for j=1,2,3, . . . ; matrix D(t|k) is defined as the matrix of bias coefficients, which linearly relates state estimation errors to the parameter errors, at time t (after processing k=0,1,2, . . . measurements); matrix D(tj|k) is denoted as D(j|k), when the time t=tj is the time of the jth measurement for j=1,2,3, . . . ; determining the time tk+1 of a new measurement and the time t when the filter was last updated; using the update interval T=tk+1−
t, determine the system transition matrices Φ and
Γ
;determining the mean value {overscore (λ
)} of unknown but bounded parameters λ
, and the input vector u({circumflex over (x)}(t|k),{overscore (λ
)});measuring aspects of the state of the system governed by the measurement equation
z(k)=Hx(k)+n(k)
where n(k) is the measurement noise with covariance N and measurement matrix H at time tk for k=1,2,3, . . . ;determining if the measurement is time-late by testing T<
0;(a) if the measurement is time-late determining F,G as follows generating a parameter matrix Λ
, representing physical bounds on the parameters λ
that are not state variables of the system;extrapolating said state estimates {circumflex over (x)}(t|k) and matrices M(t|k), D(t|k), to {circumflex over (x)}(k+1|k), M(k+1|k), D(k+1|k), and calculating S(k+1|k) as in
{circumflex over (x)}(k+1|k)=Φ
{circumflex over (x)}(t|k)+Γ
u({circumflex over (x)}(t|k),{overscore (λ
)})
M(k+1|k)=FM(t|k)F′
D(k+1|k)=FD(t|k)+G
S(k+1|k)=M(k+1|k)+D(k+1|k)Λ
D(k+1|k)′determining covariance of the residual Q as in
Q=HS(k+1|k)H′
+Ndetermining the filter gain matrix K as in
K=[M(t|k)F′
+D(t|k)Λ
D(k+1|k)′
]H′
Q−
1determining the matrix L as in
L=I−
KHF
where I is the identity matrix;updating the state estimate {circumflex over (x)}(t|k) as
{circumflex over (x)}(t|k+1)={circumflex over (x)}(t|k)+K[z(k+1)−
H{circumflex over (x)}(k+1|k)]updating the matrices M(t|k) and D(t|k) as
M(t|k+1)=LM(t|k)L′
+KNK′
D(t|k+1)=D(t|k)−
KHD(k+1|k)
respectively, and generating the total mean square error S(t|k+1) as in
S(t|k+1)=M(t|k+1)+D(t|k+1)Λ
D(t|k+1)′(b) and if the measurement is not time-late determining F,G using and, generating a parameter matrix Λ
, representing physical bounds on those parameters that are not state variables of the system;extrapolating said state estimates {circumflex over (x)}(k|k) and matrices M(k|k), D(k|k), S(k|k) to {circumflex over (x)}(k+1|k), M(k+1|k), D(k+1|k), and S(k+1|k) as in
{circumflex over (x)}(k+1|k)=Φ
{circumflex over (x)}(k|k)+Γ
u({circumflex over (x)}(k|k),{overscore (λ
)})
M(k+1|k)=FM(k|k)F′
D(k+1|k)=FD(k|k)+G
S(k+1|k)=M(k+1|k)+D(k+1|k)Λ
D(k+1|k)′determining covariance of the residual Q as in
Q=HS(k+1|k)H′
+Ndetermining the filter gain matrix K as in
K=S(k+1|k)H′
Q−
1determining the matrix L as in
L=I−
KH
where I is the identity matrix;updating the state estimate {circumflex over (x)}(k+1|k) as
{circumflex over (x)}(k+1|k+1)={circumflex over (x)}(k+1|k)+K[z(k+1)−
H{circumflex over (x)}(k+1|k)]updating the matrices M(k+1|k) and D(k+1|k) as
M(k+1|k+1)=LM(k+1|k)L′
+KNK′and,
D(k+1|k+1)=LD(k+1|k)respectively, and generating the total mean square error S(k+1|k+1) as
S(k+1|k+1)=M(k+1|k+1)+D(k+1|k+1)Λ
D(k+1|k+1)′after
- in addition to state variables x(k) at time tk for k=1,2,3, . . . , which parameters λ
-
2. A method for estimating the state of a system comprising the steps of:
-
observing a system having state variables and also having unknown, multidimensional, arbitrarily time-varying parameters, but which are subject to known bounded values and driven by a time-varying input function that depends on the states, and multidimensional parameters; measuring certain aspects of the state of the system in the presence of measurement errors to produce initial measurements; initializing state estimates and matrices using a priori information and the initial measurements; using the update interval in determining the system transition matrices and the mean value of unknown but bounded parameters and the input vector; determining if the measurement is time-late by testing the sign of the update interval; if the measurement is time-late applying the measurements to an out-of-sequence estimating filter that explicitly uses a mean square optimization criterion that separately accounts for measurement errors and said bounding values, as well as the delay time, to produce estimates of the true state of the system; if the measurement is not time-late applying the measurements to an in-sequence estimating filter that explicitly uses a mean square optimization criterion that separately accounts for measurement errors and said bounding values, to produce estimates of the true state of the system; applying said estimates to one of (a) make a decision relating to said system, (b) operate a control system, and (c) control a process.
-
Specification