Sensor fusioning with Kalman filter_问答_开发者

I'm intereste开发者_如何学Cd, how is the dual input in a sensor fusioning setup in a Kalman filter modeled?

Say for instance that you have an accelerometer and a gyro and want to present the "horizon level", like in an airplane, a good demo of something like this here.

How do you actually harvest the two sensors positive properties and minimize the negative?

Is this modeled in the Observation Model matrix (usually symbolized by capital H)?

Remark: This question was also asked without any answers at math.stackexchange.com

Usually, the sensor fusion problem is derived from the bayes theorem. Actually you have that your estimate (in this case the horizon level) will be a weighted sum of your sensors, which is caracterized by the sensor model. For dual sensors, you have two common choices: Model a two sensor system and derive the kalman gain for each sensor (using the system model as the predictor), or run two correction stages using different observation models. You should take a look at Bayesian Predictors (a little more general than Kalman Filter) which is precisely derived from minimizing the variance of an estimate, given two different information sources. If you have a weighted sum, and minimize the variance of the sum, for two sensors, then you get the Kalman Gain.

The properties of the sensor can be "seen" in two parts of the filter. First, you have the error matrix for your observations. This is the matrix that represents the noise in the sensors observation (it is assumed to be zero mean gaussian noise, which isn't a too big assumption, given that during calibration, you can achieve a zero mean noise).

The other important matrix is the observation covariance matrix. This matrix gives you an insight about how good is the sensor at giving you information (information meaning something "new" and not dependent on the other sensors reading).

About "harvesting the good characteristics", what you should do is do a good calibration and noise characterization (is that spelled ok?) of the sensors. The best way to get a Kalman Filter to converge is to have a good noise model for your sensors, and that is 100% experimental. Try to determine the variance for your system (dont always trust datasheets).

Hope that helps a bit.

The gyro measures rate of angle change (e.g. in radians per sec), while from accelerometer reading you can calculate the angle itself. Here is a simple way of combining these measurements:

At every gyro reading received:

angle_radians+=gyro_reading_radians_per_sec * seconds_since_last_gyro_reading

At every accelerometer reading received:

angle_radians+=0.02 * (angle_radians_from_accelerometer - angle_radians)

The 0.02 constant is for tuning - it selects the tradeoff between noise rejection and responsiveness (you can't have both at the same time). It also depends on the accuracy of both sensors, and the time intervals at which new readings are received.

These two lines of code implement a simple 1-dimensional (scalar) Kalman filter. It assumes that

the gyro has very low noise compared to accelerometer (true with most consumer-grade sensors). Therefore we do not model gyro noise at all, but instead use gyro in the state transition model (usually denoted by F).
accelerometer readings are received at generally regular time intervals and accelerometer noise level (usually R) is constant
angle_radians has been initialised with an initial estimate (f.ex by averaging angle_radians_from_accelerometer over some time)
therefore also estimate covariance (P) and optimal Kalman gain (K) are constant, which means we do not need to keep estimate covariance in a variable at all.

As you see, this approach is simplified. If the above assumptions are not met, you should learn some Kalman filter theory, and modify the code accordingly.

Horizon line is G' * (u, v, f)=0 ,where G is a gravity vector, u and v image centred coordinates and f focal length. Now pros and cons of sensors: gyro is super fast and accurate but drifts, accelerometer is less accurate but (if calibrated) has zero bias and doesn't drift (given no acceleration except gravity). They measure different things - accelerometer measures acceleration and thus orientation relative to the gravity vector while gyro measures rotation speed and thus the change in orientation. To convert it to orientation one has to integrate its values (thankfully it can be sampled at high fps like 100-200). thus Kalman filter that supposed to be linear is not applicable to gyro. for now we can just simplify sensor fusion as a weighted sum of readings and predictions.

You can combine two readings - accelerometer and integrated gyro and model prediction using weights that are inversely proportional to data variances. You will also have to use compass occasionally since accelerometer doesn't tell you much about the azimuth but I guess it is irrelevant for calculation of a horizon line. The system should be responsive and accurate and for this purpose whenever orientation changes fast the weights for gyro should be large; when the system settles down and rotation stops the weights for accelerometer will go up allowing more integration of zero bias readings and killing the drift from gyro.