Peter S. Maybeck – “Stochastic models, estimation, and control” Greg Welch et Al. –...
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Transcript of Peter S. Maybeck – “Stochastic models, estimation, and control” Greg Welch et Al. –...
Peter S. Maybeck – “Stochastic models, estimation, and control”Greg Welch et Al. – ”Introduction to the Kalman filter”Sebastian Thrun, Udacity. “Artificial Intelligence for Robotics –Kalman Filters”Micheal Williams - “KalmanFilters” , http://users.cecs.anu.edu.au/~hartley/Vision-Reading-Course/Kalman-filters.ppt
4. FEBUAR 2014
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
LESSON 2 – KALMAN FILTERS
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 20142
AGENDA›Applications›What is a Kalman Filter›Conceptual Overview›Design Kalman Filter›Example ›Demo MATLAB
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
APPLICATIONS›Tracking Objects › Missiles › Lip reading› Hands
›Economics
›Navigation (Google car)
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
WHAT IS A KALMAN FILTER›Recursive data processing algorithm
›Recursive?› KF does not require all previous data to be kept in storage
›Kalman filter finds the most optimum averaging factor for each consequent state. Also somehow remembers a little bit about the past states
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
PREVIOUS LESSON›Monte Carlo localization › World divided info discrete grids› Approximates the posterior distribution as histogram
›Now we look at KF› The posterior distribution is given by a Gaussian› Gaussian is a cont. Function › Area underneath sums to one
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
CONCEPTUAL OVERVIEW›Lost on the 1D line
› A measurement at t1: Mean = z1 and Variance = 2z1
› Optimal estimate of position is: (t1) = z1
› Variance of error in estimate: 2x (t1) = 2
z1
› Boat in same position at time t2
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
› So we have the prediction -(t2)› Better Measurement at t2: Mean = z2 and Variance = z2
› Need to correct the prediction due to measurement to get (t2)› Closer to more trusted measurement
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CONCEPTUAL OVERVIEW
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prediction -(t2)measurement z(t2)
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
CONCEPTUAL OVERVIEW
› Corrected mean is the new optimal estimate of position› New variance is smaller than either of the previous two variances
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measurement z(t2)
prediction -(t2)
corrected optimal estimate (t2)
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
CONCEPTUAL OVERVIEW
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› Optimal estimate (t2) = µ
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2 2 2 2
2 2 2 22 2
2 2 2 2
2 2 2
2 2
2 2
2 2 2 2
xz
x z x z
z x x xz x
x z x z
x z x
x z
x x
x z x z
x x z
x z x xx z
x z x
x z x x K z x K
: prediction (a priori estimate): update (a posteriori estimate)K: Kalman gain
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
CONCEPTUAL OVERVIEW
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› At time t3, boat moves with velocity dx/dt=u› Naïve approach: Shift probability to the right to predict› This would work if we knew the velocity exactly (perfect model)
Naïve Prediction -(t3)(t2)
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
› Better to assume imperfect model by adding Gaussian noise› dx/dt = u + w› u= nominal velocity› w= noise term or uncertainty (variance)› Distribution for prediction moves and spreads out
CONCEPTUAL OVERVIEW
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(t2)Naïve Prediction -(t3)
Prediction -(t3)
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
› Now we take a measurement at t3
› Need to once again correct the prediction› Same as before
CONCEPTUAL OVERVIEW
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Prediction -
(t3)
Measurement z(t3)
Corrected optimal estimate (t3)
3 2 3 2
2 2 23 2 3 2
( ) ( ) ( )
( ) ( ) ( )x x w
x t x t u t t
t t t t
3 3 3 3 3
2 2 23 3 3 3
23
3 2 23 3
( ) ( ) ( )( ( ))
( ) ( ) ( ) ( )
( )( )
( )
x x x
x
x z
x t x t K t z x t
t t K t t
tK t
t
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
DESIGN KALMAN FILTERS
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
DESIGN KALMAN FILTERS
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› Process to be estimated: (state space)
› Kalman Filter
xk = Axk-1 + Buk + wk-1
zk = Hxk + vk
Process Noise (w) with covariance Q
Measurement Noise (v) with covariance R
Prediction: - is estimate based on measurements at previous time-steps
k = -k + K(zk - H -
k )
Correction: k has additional information – the measurement at time k
K = P-kHT(HP-
kHT + R)-1
-k = Axk-1 + Buk
P-k = APk-1AT + Q
Pk = (I - KH)P-k
P-k: Prior error covariance
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
DESIGN KALMAN FILTERS
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
DESIGN KALMAN FILTERS
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
› Consider an object falling under a constant gravitational field. Let y(t) denote the height of the object, then:
y t g
0 0y t y t g t t
2
0 0 0 02
gy t y t y t t t t t
0Discrete time system with 1t t t
1 1 12
gy k y k g y k y k y k
KALMAN FILTERS - EXAMPLE
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LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
› Construct state space model from equations, when we are able to perform measurements, zk, of the height.
that is, find A, B, uk and H in:
KALMAN FILTERS - EXAMPLE
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1 1 12
gy k y k g y k y k y k
xk = Axk-1 + Buk
zk = Hxk
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
› Construct state space model from equations, when we are able to perform measurements, zk, of the height.
Solution:
KALMAN FILTERS - EXAMPLE
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1 1 12
gy k y k g y k y k y k
1
11
1 1 0.5
0 1 1
1 0
k k
k kk k
k k kk
k
y yg
y yA B
H yz
y
x x u
z x
A B
H
uXk-1Xk
Xkzk
LESSON2 – KALMAN FILTERSJESPER JESSEN, 201300253
4. FEBUAR 2014
EXAMPLE›MATLAB demo
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