卡尔曼滤波器【Kalman Filter For Dummies】

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A Quick Insight

As I mentioned earlier, it's nearly impossible to grasp the full meaning of Kalman Filter by starting from definitions and complicated equations (at least for us mere mortals). For most cases, the state matrices drop out and we obtain the below equation, which is much easier to start with.

Remember, the k's on the subscript are states. Here we can treat it as discrete time intervals, such as k=1 means 1ms, k=2 means 2ms.

Our purpose is to find , the estimate of the signal x. And we wish to find it for each consequent k's.

Also here, is the measurement value. Keep in mind that, we are not perfectly sure of these values. Otherwise, we won't be needing to do all these. And is called "Kalman Gain" (which is the key point of all these), and is the estimate of the signal on the previous state.

The only unknown component in this equation is the Kalman Gain . Because, we have the measurement values, and we already have the previous estimated signal. You should calculate this Kalman Gain for each consequent state. This is not easy of course, but we have all the tools to do it.

On the other hand, let's assume to be 0.5, what do we get? It's a simple averaging! In other words, we should find smarter coefficients at each state. The bottom line is :

Kalman filter finds the most optimum averaging factor for each consequent state. Also somehow remembers a little bit about the past states.

Isn't this amazing?

Step-by-Step Guide

Here's a simple step-by-step guide for a quick start to Kalman filtering.

STEP 1 - Build a Model

It's the most important step. First of all, you must be sure that, Kalman filtering conditions fit to your problem.

As we remember the two equations of Kalman Filter is as follows:

It means that each x_k  (our signal values) may be evaluated by using a linear stochastic equation (the first one). Any x_k is a linear combination of its previous value plus a control signal u_k and a process noise (which may be hard to conceptualize). Remember that, most of the time, there's no control signal u_k.

The second equation tells that any measurement value (which we are not sure its accuracy) is a linear combination of the signal value and the measurement noise. They are both considered to be Gaussian.

The process noise and measurement noise are statistically independent.

The entities A, B and H are in general form matrices. But in most of our signal processing problems, we use models such that these entities are just numeric values. Also as an additional ease, while these values may change between states, most of the time, we can assume that they're constant.

If we are pretty sure that our system fits into this model (most of the systems do by the way), the only thing left is to estimate the mean and standard deviation of the noise functions W_k-1 and v_k. We know that, in real life, no signal is pure Gaussian, but we may assume it with some approximation. This is not a big problem, because we'll see that the Kalman Filtering Algorithm tries to converge into correct estimations, even if the Gaussian noise parameters are poorly estimated.

The only thing to keep in mind is : "The better you estimate the noise parameters, the better estimates you get."

STEP 2 - Start the Process

If you succeeded to fit your model into Kalman Filter, than the next step is to determine the necessary parameters and your initial values.

We have two distinct set of equations : Time Update (prediction) and Measurement Update (correction). Both equation sets are applied at each k^th state.

Time Update (prediction)	Measurement Update (correction)

We made the modeling in STEP1, so we know the matrices A, B and H. Most probably, they will be numerical constants. And even most probably, they'll be  equal to 1. I suggest you to re-write these equations and see how simplified will these equations become. (if you're lazy enough not to do it, I'll do it for you in the Example below).

The most remaining painful thing is to determine R and Q. R is rather simple to find out, because, in general, we're quite sure about the noise in the environment. But finding out Q is not so obvious. And at this stage, I can't give you a specific method.

To start the process, we need to know the estimate of x₀, and P₀.

STEP 3 - Iterate

After we gathered all the information we need and started the process, now we can iterate through the estimates. Keep in mind that the previous estimates will be the input for the current state.

Here, is the "prior estimate" which in a way, means the rough estimate before the measurement update correction. And also  is the "prior error covariance". We use these "prior" values in our Measurement Update equations.

In Measurement Update equations, we really find which is the estimate of x at time k (the very thing we wish to find). Also, we find which is necessary for the k 1 (future) estimate, together with . The Kalman Gain () we evaluate is not needed for the next iteration step, it's a hidden, mysterious and the most important part of this set of equations.

The values we evaluate at Measurement Update stage are also called "posterior" values. Which also makes sense.

Answers to Silly Questions

Can I deploy Kalman Filter to all Digital Signal Processing problems?

I've seen lots of papers that use Kalman Filter for a variety of problems, such as noise filtering, sub-space signal analysis, feature extraction and so on. The bottom line is, you can use Kalman Filter with a quite approximation and clever modeling.

Can I use it for Image Processing?

Of course.

Where do we find these Time Update and Measurement Update equations? It seems that they suddenly appeared from nowhere.

You can derive it from the linear stochastic difference equation (the equations in STEP 1), by taking the partial derivative and setting them to zero (for minimizing the estimation error). Of course they're hard and time consuming.

	Rudolf Emil Kalman

Rudolf Kalman was born in Budapest, Hungary, and obtained his bachelor's degree in 1953 and master's degree in 1954 from MIT in electrical engineering. His doctorate in 1957 was from Columbia University.

Kalman is an electrical engineer by training, and is famous for his co-invention of the
Kalman filter, a mathematical technique widely used in control systems and avionics to extract a
signal from a series of incomplete and noisy measurements.

Kalman's ideas on filtering were initially met with skepticism, so much so that he was
forced to first publish his results in a mechanical (rather than electrical) engineering journal.

He had more success in presenting his ideas, however, while visiting Stanley F. Schmidt at the
NASA Ames Research Center in 1960. This led to the use of Kalman filters during the Apollo program.

A Simple Example

Now let's try to estimate a scalar random constant, such as a "voltage reading" from a source. So let's assume that it has a constant value of aV (volts) , but of of course we some noisy readings above and below a volts. And we assume that the standard deviation of the measurement noise is 0.1 V.

Now let's build our model:

As I promised earlier, we reduced the equations to a very simple form.

• Above all, we have a 1 dimensional signal problem, so every entity in our model is a numerical value, not a matrix.

• We have no such control signal u_k, and it's out of the game

• As the signal is a constant value, the constant A is just 1, because we already know that the next value will be same as the previous one. We are lucky that we have a constant value in this example, but even if it were any other linear nature, again we could easily assume that the value A will be 1.

• The value H = 1, because we know that the measurement is composed of the state value and some noise. You'll rarely encounter real life cases that H is different from 1.

And finally, let's assume that we have the following measurement values:

TIME (ms)	1	2	3	4	5	6	7	8	9	10
VALUE (V)	0.39	0.50	0.48	0.29	0.25	0.32	0.34	0.48	0.41	0.45

OK, we should start from somewhere, such as k=0. We should find or assume some initial state. Here, we throw out some initial values. Let's assume estimate of X₀ = 0, and P₀ = 1. Then why didn't we choose P₀ = 0 for example? It's simple. If we chose that way, this would mean that there's no noise in the environment, and this assumption would lead all the consequent to be zero(remaining as the initial state). So we choose P₀ something other that zero.

Let's write the Time Update and Measurement Update equations.

Time Update (prediction)	Measurement Update (correction)

Now, let's calculate the values for each iteration.

k	1	2	3	4	5	6	7	8	9	10
	0.390	0.500	0.480	0.290	0.250	0.320	0.340	0.480	0.410	0.450
	0	0.355	0.424	0.442	0.405	0.375	0.365	0.362	0.377	0.380
	1	0.091	0.048	0.032	0.024	0.020	0.016	0.014	0.012	0.011
Time Update	= = 0 = = 1	= 0.355 = 0.091
Measurement Update	= 1 / (1 0.1) = 0.909 = 0 0.909 (0.390 - 0) = 0.35 = (1 - 0.909) . 1 = 0.091	= 0.091 / (0.091 0.1) = 0.476 = 0.355 0.476 (0.500 - 0.355) = 0.424 = (1 - 0.476) . 0.091 = 0.048
	0.355	0.424	0.442	0.405	0.375	0.365	0.362	0.377	0.380	0.387
	0.091	0.048	0.032	0.024	0.020	0.016	0.014	0.012	0.011	0.010

Here, I displayed the first 2 state iterations in detail, the others follow the same pattern. I've completed the other numerical values via a computer algorithm, which is the appropriate solution. If you try to write it as an algorithm, you'll discover that Kalman Filter is very easy to implement. The chart here (right) shows that the Kalman Filter algorithm converges to the true voltage value. Here, I displayed the first 10 iterations and we clearly see the signs of convergence. In 50 or so iterations, it'll converge even better. To enable the convergence in fewer steps, you should • Model the system more elegantly • Estimate the noise more precisely OK. We're done. The only thing to do is collecting the values we've calculated. That's it!

The Kalman Filter algorithm converges to the truth over a few iterations

References

[1] Greg Welch, Gary Bishop, "An Introduction to the Kalman Filter",  University of North Carolina at Chapel Hill Department of Computer Science, 2001

[2] M.S.Grewal, A.P. Andrews, "Kalman Filtering - Theory and Practice Using MATLAB", Wiley, 2001