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Using the Kalman Filter to Estimate the state of a Maneuvering Aircraft Prepared By: Kevin Meier Alok Desai 11/29/2011 ECEn -670 Stochastic Process 1 ECEn -670 Stochastic Process Instructor: Dr. Brian Mazzeo

U sing the Kalman Filter to Estimate the state of a Maneuvering Aircraft

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U sing the Kalman Filter to Estimate the state of a Maneuvering Aircraft . Prepared By: Kevin Meier Alok Desai. ECEn -670 Stochastic Process. Instructor: Dr. Brian Mazzeo. Outlines. Kalman filter Correlation Between the Process and Measurement Noise - PowerPoint PPT Presentation

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Page 1: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

Using the Kalman Filter to Estimate the state of a Maneuvering Aircraft

Prepared By: Kevin Meier Alok Desai

11/29/2011 ECEn -670 Stochastic Process 1

ECEn -670 Stochastic Process

Instructor: Dr. Brian Mazzeo

Page 2: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 2

Outlines

• Kalman filter• Correlation Between the Process and

Measurement Noise• Application of KF for estimating Bearing and

Range• Simulation results

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Page 3: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 3

Kalman Filter

• Purpose: It is to use measurements observed over time, containing noise (random variations) and other inaccuracies, and produce values that tend to be closer to the true values of the measurements and their associated calculated values.

• When system model and measurement model equations are linear, then to estimate the state vector recursively.

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Page 4: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 4

Estimating States

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• System dynamic model:

• Measurement model:

Page 5: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 5

Kalman Filter Estimation

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Page 6: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 6

Kalman Filter (Cont.)

• State estimation: • Error covariance (a priori):

• Kalman Gain:• Error covariance update (a posteriori):

• State estimate update:

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Page 7: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 7

Correlation Between the Process and Measurement Noise

• Correlation be given by• Prediction equation remain unchanged.• Measurement equation

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Page 8: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 8

Range and Bearing Estimation

• Radars are used to track aircraft.

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Page 9: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 9

• Range = ct/2

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Page 10: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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How the Kalman filter applies to Radar

• Radar is used to track the state of an aircraft• The state is the range, range rate, bearing and

bearing rate

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Page 11: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 11

How to model the aircraft with no acceleration data

• Model the acceleration as a uniform random variable using the singer model. Where the acceleration is correlated from sample to sample

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Page 12: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 12

How the Kalman filter applies to Radar

• The radar uses sensors to measure the Range and Bearing angle. In this process there is sensor measurement noise

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Page 13: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 13

How the Kalman filter applies to Radar

• The process and measurement noise are zero-mean white Gaussian random variables

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Page 14: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 1411/29/2011

Page 15: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Error Covariance for Range

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Error covariance (One prediction) Error covariance (Multiple prediction)

Page 16: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

ECEn -670 Stochastic Process 16

Error Covariance of Bearing

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Error covariance (One prediction) Error covariance (Multiple prediction)

Page 17: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Bearing Angle

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Bearing Angle (One prediction) Bearing Angle (Multiple prediction)

Page 18: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Vehicle Range

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Vehicle Range (One Prediction) Vehicle Range (Multiple Prediction)

Page 19: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Range Error

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Range Error (One Prediction)c

Vehicle Range (Multiple Prediction)

Page 20: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Bearing Rate

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Bearing ( one prediction ) Bearing (multiple prediction )

Page 21: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Range

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Range (One prediction ) Range (Multiple prediction )

Page 22: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Range Error and Range Ratewith correlated noise

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Range Error Range Rate

Page 23: U sing the  Kalman  Filter  to Estimate the state of a Maneuvering  Aircraft

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Questions??

Thank you !

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