IP Library Granted Patent US 7,928,898
Granted Patent B2
US 7,928,898 · App. 12/527,146 · Granted Apr 19, 2011

Method for determining the kinematic state of an object, by evaluating sensor measured values

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,928,898
App. No.
12/527,146
Granted
Apr 19, 2011
Kind
B2
Abstract

In a method for determining the kinematic state of an object by evaluating a sequence of discrete polar measured values of a sensor, the polar measurements r m , α m are converted to Cartesian coordinates and subsequently scaled to Cartesian pseudo-measurements using a scaling factor β calculated as a function of measured range r m . Associated pseudo-measurement error variance matrices are determined, each comprising nominal measurement error variances in the range direction R 2 m and transversely thereto C 2 m as a function of the measured range r m . The state of the object is estimated, with an estimated variance {circumflex over (σ)} 2 cross being determined transversely with respect to the range direction in an estimation device, based on the Cartesian pseudo-measurements and the pseudo-measurement error variance matrices. The scaling factor β is chosen such that no systematic error results for a position estimate comprising n>1 measurements; and the nominal pseudo-measurement error variance R 2 m in the range direction is calculated as a function of the nominal pseudo-measurement error variance C 2 m transversely thereto or conversely such that the variance {circumflex over (σ)} 2 cross which is estimated after processing of n>1 measurements, transversely with respect to the range direction, on average matches the actual variance {circumflex over (σ)} 2 cross of the estimated error transversely with respect to the range direction.

Claims (17)

1. A method for determining a kinematic state of an object, including at least one of position, velocity and acceleration of the object, said method comprising:

a sensor making a sequence of discrete polar measurements with respect to said object, said polar measurements including as polar measurement variables, range and azimuth measurements from said sensor to said object;

converting the polar measurements to Cartesian coordinates by conversion of the polar measurement variables range and azimuth;

scaling the Cartesian coordinates to Cartesian pseudo-measurements using a scaling factor β which is determined as a function of measured range;

determining associated nominal pseudo-measurement error variance matrices, each comprising specific nominal pseudo-measurement error variances (R 2 m ) in a range direction and transversely thereto (C 2 m ), as a function of the measured range; and

based on the Cartesian pseudo-measurements and the associated nominal pseudo-measurement error variance matrices, an estimation unit estimating the kinematic state of the object, with an estimated variance {circumflex over (σ)} 2 cross being determined transversely with respect to the range direction; wherein,

the scaling factor β is determined in the estimation device such that no systematic error results for a position estimate comprising n>1 measurements; and

the nominal pseudo-measurement error variance R 2 m in the range direction is determined in the estimation device as a function of the nominal pseudo-measurement error variance C 2 m transversely to the range direction, or such that the variance {circumflex over (σ)} 2 cross which is estimated after the processing of n>1 measurements, transversely with respect to the range direction, on average matches the actual variance {circumflex over (σ)} 2 cross of the estimated error transversely with respect to the range direction.

2. The method as claimed in claim 1 , wherein:

a desired variance of the position estimate transversely with respect to the range direction is defined by presetting a reference value {circumflex over (σ)} 2 ref ; and

the nominal variances are determined in the range direction (R 2 m ) and transversely thereto (C 2 m ) such that the estimation device on average determines position estimates with desired variances transversely with respect to the range direction, and produces matching estimates.

3. The method as claimed in claim 2 , wherein a reference value {circumflex over (σ)} 2 ref is determined such that a bias-free method is achieved by the associated nominal variances in the range direction (R 2 ref ) and transversely thereto (C 2 ref ) with a consistent estimate of the estimated error variance transversely with respect to the range direction, with minimized nominal variance of the psuedo-measurements in the range direction.

4. The method as claimed in claim 3 , wherein R 2 ref is calculated:

in a first step, with the reference value {circumflex over (σ)} 2 ref being determined such that a bias-free method is specified by the associated nominal variances in the range direction (R 2 ref ) and transversely thereto (C 2 ref ), with a consistent estimate of the estimated error variance transversely with respect to the range direction, and with nominal variance of the psuedo-measurements in the range direction being as small as possible; and

in a second step, the reference variable R 2 ref multiplied by a real factor q is used as the nominal variance R 2 m in the range direction.

5. The method as claimed in claim 4 , wherein the factor q is greater than unity.

6. The method as claimed in claim 5 , wherein the factor q is limited by a value q max .

Assignments (7)
CORRECTIVE ASSIGNMENT TO CORRECT THE PATENT NUMBER FROM 9476976 TO 9476967 PREVIOUSLY RECORDED AT REEL: 48284 FRAME: 766. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Apr 15, 2020
From: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
To: HENSOLDT SENSORS GMBH
Reel/Frame 052534/0259 →
CORRECTIVE ASSIGNMENT TO CORRECT THE PATENT NUMBER PAT. NO.9476976 PREVIOUSLY RECORDED ON REEL 047691 FRAME 0890. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT OF ASSIGNORS INTEREST. Recorded Jun 18, 2019
From: AIRBUS DEFENCE AND SPACE GMBH
To: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
Reel/Frame 049499/0724 →
CHANGE OF NAME Recorded Feb 7, 2019
From: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
To: HENSOLDT SENSORS GMBH
Reel/Frame 048284/0766 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2018
From: AIRBUS DEFENCE AND SPACE GMBH
To: AIRBUS DS ELECTRONICS AND BORDER SECURITY GMBH
Reel/Frame 047691/0890 →
CHANGE OF ADDRESS Recorded Mar 30, 2017
From: AIRBUS DEFENCE AND SPACE GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 042114/0218 →
CHANGE OF NAME Recorded Jan 20, 2017
From: EADS DEUTSCHLAND GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 041440/0239 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 19, 2009
From: FRAENKEN, DIETRICH
To: EADS DEUTSCHLAND GMBH
Reel/Frame 023543/0932 →