STATE ESTIMATION APPARATUS

• US 20130110451A1
• Filed: 10/26/2012
• Published: 05/02/2013
• Est. Priority Date: 10/28/2011
• Status: Abandoned Application

• Current Assignee: Yamaha Corporation
• Original Assignee: Yamaha Corporation
• Inventors: Handa, Ibuki
• Application Number:
  US13/661,244
• Publication Number:
  US 20130110451A1
• Time in Patent Office: Days
• US Class Current: 702/141
• CPC Class Codes: G01V 3/40 specially adapted for measuring magnetic field characteristics of the earth

Abstract

A state estimation apparatus is mounted in a portable instrument having a part generating a magnetic field. The state estimation apparatus is provided with a magnetic sensor and an acceleration sensor. A stability decision module decides whether motion of the portable instrument is stable or not. A Kalman filter operation module sets an initial vector to a state vector of Kalman filter as an initial value thereof in case that the stability decision module decides that the motion of the portable instrument is stable, and then updates the state vector using an observed value vector having outputs the magnetic sensor and the acceleration sensor, the initial vector having as components thereof an estimated value of an offset representing the magnetic field generated by the part of the instrument and a vector estimating a posture of the portable instrument.

Claims

1. A state estimation apparatus mounted in an instrument comprising a part generating a magnetic field, the state estimation apparatus comprising:

a three-dimensional magnetic sensor that detects magnetic components in three directions perpendicular to each other and sequentially outputs magnetic data as three-dimensional vector data expressed in a three axis coordinate system;

a three-dimensional acceleration sensor that detects acceleration at three axes perpendicular to each other and sequentially outputs acceleration data as three-dimensional vector data expressed in a three axis coordinate system;

a stability decision module that decides whether motion of the instrument is stable or not; and

a Kalman filter operation module that sets an initial vector to a state vector of Kalman filter as an initial value thereof in case that the stability decision module decides that the motion of the instrument is stable, and then updates the state vector of Kalman filter using an observed value vector having outputs of a plurality of sensors being mounted in the instrument and including the three-dimensional magnetic sensor and the three-dimensional acceleration sensor, the initial vector having as components thereof an estimated value of an offset representing the magnetic field generated by the part of the instrument and a vector estimating a posture of the instrument.

2. The state estimation apparatus according to claim 1, further comprising an initial vector generation module that generates the initial vector in case that the stability decision module decides that the motion of the instrument is stable.

3. The state estimation apparatus according to claim 2, wherein the initial vector generation module generates the initial vector based on the magnetic data, the acceleration data, and three axis coordinates of a central point of a plurality of magnetic data, the central point indicating an approximate value of the offset of the three-dimensional magnetic sensor.

4. The state estimation apparatus according to claim 3, further comprising:

an accumulation module that accumulates the magnetic data sequentially output from the three-dimensional magnetic sensor; and

a central point calculation module that calculates the three axis coordinates of the central point based on the plurality of magnetic data accumulated in the accumulation module.

5. The state estimation apparatus according to claim 4, further comprising a first notification part that urges a user to change the posture of the instrument before the central point calculation module starts to acquire the plurality of magnetic data used to calculate the central point.

6. The state estimation apparatus according to claim 5, further comprising a second notification part for urging the user not to change the posture of the instrument after the central point calculation module calculates the central point.

7. The state estimation apparatus according to claim 1, wherein the stability decision module decides whether the motion of the instrument is stable or not based on the plurality of acceleration data output from the three dimensional acceleration sensor.

8. The state estimation apparatus according to claim 7, wherein the stability decision module comprises a low pass filter for calculating reference acceleration data based on the plurality of acceleration data, calculates stability indices representing errors between three axis coordinates indicated by the acceleration data and three axis coordinates indicated by the reference acceleration data with respect to a predetermined number of the acceleration data, and decides that the motion of the instrument is stable in case that all of the stability indices are equal to or less than a first threshold value.

9. The state estimation apparatus according to claim 7, wherein the stability decision module calculates a variance of the three axis coordinates indicated by a predetermined number of the acceleration data as a stability index, and decides that the motion of the instrument is stable in case that the stability index is equal to or less than a second threshold value.

10. A control method of a state estimation apparatus mounted in an instrument comprising a part generating a magnetic field, the state estimation apparatus including a three-dimensional magnetic sensor that detects magnetic components in three directions perpendicular to each other and sequentially outputs magnetic data as three-dimensional vector data expressed in a three axis coordinate system, and a three-dimensional acceleration sensor that detects acceleration at three axes perpendicular to each other and sequentially outputs acceleration data as three-dimensional vector data expressed in a three axis coordinate system, the control method comprising:

a stability decision step of deciding whether motion of the instrument is stable or not; and

a Kalman filter operation step of setting an initial vector to a state vector of Kalman filter as an initial value thereof in case that the stability decision step decides that the motion of the instrument is stable, and then updating the state vector of Kalman filter using an observed value vector having outputs of a plurality of sensors being mounted in the instrument and including the three-dimensional magnetic sensor and the three-dimensional acceleration sensor, the initial vector having as components thereof an estimated value of an offset representing the magnetic field generated by the part of the instrument and a vector estimating a posture of the instrument.