Coordinate detecting apparatus having acceleration detectors

• US 5,587,558 A
• Filed: 01/21/1993
• Issued: 12/24/1996
• Est. Priority Date: 01/24/1992
• Status: Expired due to Term

• Current Assignee: Seiko Instruments Incorporated (Seiko Group)
• Original Assignee: Seiko Instruments Incorporated (Seiko Group)
• Inventors: Matsushima, Kenichi
• Primary Examiner(s): Chin, Wellington
• Assistant Examiner(s): Shankar, Vijay
• Application Number:
  US08/007,072
• Time in Patent Office: 1,433 Days
• Field of Search: 178/18, 178/19, 178/20, 345/156, 345/157, 345/173, 345/174, 345/175, 345/179, 345/180
• US Class Current: 178/18.01
• CPC Class Codes: G06F 3/0346 with detection of the device orientation or free movement in a 3D space, e.g. 3D mice, 6-DOF [six degrees of freedom] pointers using gyroscopes, accelerometers or tilt-sensors
• CPC Class Codes: G06F 3/03545 Pens or stylus

Abstract

A coordinate input device includes a coordinate detector which may include an acceleration detector for accurate determination of the spatial coordinates of a coordinate indicator. A three-dimensional acceleration in a first coordinate system is detected by a first acceleration detecting unit and is converted into an input coordinate system in accordance with the attitude of the coordinate indicator. The effect of gravity is removed and the acceleration is integrated to obtain the spatial coordinates of the coordinate indicator. Even if the coordinate indicator is tilted, accurate coordinate input can be performed.

Claims

1. A coordinate input device for obtaining the spatial coordinates at the tip of a pen-type coordinate indicator, comprising:

acceleration detecting means for detecting the acceleration of a body of the pen-type coordinate indicator;

attitude detecting means for detecting the attitude of the body of the pen-type coordinate indicator; and

coordinate operation means for determining the spatial coordinates at the tip of the coordinate indicator in accordance with outputs of the acceleration detecting means and the attitude detecting means.

2. A coordinate input device according to claim 1;

wherein the coordinate operation means comprises first coordinate converting means for performing coordinate transformation on an input signal using an output signal of the attitude detecting means, gravity compensation means for removing the effect of gravity with respect to the input signal, and first integrating means for integrating the input signal to convert it into the spatial coordinates at the tip of the coordinate indicator.

3. A coordinate input device according to claim 1;

wherein the attitude detecting means comprises angular acceleration detecting means for detecting an angular acceleration of the coordinate indicator, second integrating means for converting an angular acceleration signal output by the angular acceleration detecting means into an angular velocity signal or angular information and direction operation means for converting the angular velocity signal or angular information into the attitude of the body of the pen-type coordinate indicator.

4. A coordinate input device according to claim 2;

further comprising second coordinate converting means for performing coordinate transformation of the spatial coordinates output by the first integrating means using the output of the attitude detecting means.

5. A coordinate input device according to claim 1;

wherein an acceleration detector included in the acceleration detecting means serves as an acceleration detector included in the attitude detecting means.

6. A coordinate input device according to claim 1;

wherein the attitude detecting means comprises an angular acceleration detecting means in which at least two sets of acceleration detectors, each set of which comprises a pair of parallel acceleration detectors, are arranged to correspond to the axes in which the coordinate indicator detects an input signal independently in each axis for at least two-directional acceleration, integrating means for receiving an output from the angular acceleration detecting means and outputting velocity signals corresponding respectively to the outputs of the acceleration detectors, subtraction means for subtracting one of the velocity signals from the other corresponding to the outputs of the acceleration detectors to obtain an angular velocity signal, and direction operation means for converting the angular velocity signal into information representative of the attitude of the coordinate indicator.

7. A coordinate input device according to claim 1;

wherein the attitude detecting means comprises acceleration detecting means for detecting three-dimensional accelerations at three points within the body of a coordinate indicator, the three points not being on the same straight line, integrating means for obtaining the coordinates at the three points using the output from the acceleration detecting means, and direction operation means for obtaining the difference between the coordinates at the three points to determine the attitude of the coordinate indicator.

8. A coordinate input device according to claim 1;

wherein the attitude detecting means comprises angular velocity detecting means for detecting an angular velocity of the coordinate indicator;

direction operation means for determining the attitude of the coordinate indicator using the output from the angular velocity detecting means;

acceleration detecting means for detecting the acceleration of the coordinate indicator;

coordinate converting means for performing coordinate transformation of a detected acceleration of the coordinate indicator or gravity acceleration using the attitude output from the direction operation means;

gravity compensation means for removing an effect of gravity from the detected acceleration of the coordinate indicator; and

filter means for removing a dynamic component from the detected acceleration of the coordinate indicator.

9. A coordinate input device for inputting the spatial coordinates of a coordinate indicator using an acceleration detector, the coordinate input device comprising:

a coordinate indicator for indicating an input coordinate;

acceleration detecting means fixed in the coordinate indicator for detecting an acceleration of the coordinate indicator;

first integrating means for integrating the acceleration output by the acceleration detecting means and for obtaining a velocity of the coordinate indicator;

second integrating means for integrating the velocity output by the first integrating means and for obtaining the position of the coordinate indicator; and

negative feedback means for performing a negative feedback function from the output of the second integrating means to the input of the first integrating means.

10. A coordinate input device for inputting the spatial coordinates of a coordinate indicator using an acceleration detector, the coordinate input device comprising:

a coordinate indicator for indicating an input coordinate;

acceleration detecting means fixed in the coordinate indicator for detecting an acceleration of the coordinate indicator;

first integrating means for integrating the acceleration output by the acceleration detecting means and for obtaining a velocity of the coordinate indicator;

second integrating means for integrating the velocity output by the first integrating means and for obtaining the position of the coordinate indicator; and

at least one of a negative feedback means for performing a negative feedback function from the output of the first integrating means to the input of the first integrating means or a negative feedback means for performing a negative feedback function from the output of the second integrating means to the input of the second integrating means.

11. A coordinate input device for calculating the spatial coordinates at the tip of a pen-type coordinate indicator, the coordinate input device comprising:

coordinate detecting means for determining the spatial coordinates of a pen-type coordinate indicator in a first coordinate system;

attitude detecting means for determining the attitude of a body of the coordinate indicator; and

first coordinate conversion means for determining the spatial coordinates at the tip of the coordinate indicator in a second coordinate system in accordance with the spatial coordinates of the coordinate indicator body in the first coordinate system and the attitude of the coordinate indicator body.

12. A coordinate input device according to claim 11;

wherein the coordinate detecting means comprises acceleration detecting means for detecting the acceleration of the coordinate indicator in at least two dimensions and integrating means for integrating and converting the detected acceleration into the spatial coordinates of the coordinate indicator.

13. A coordinate input device according to claim 12;

wherein the coordinate detecting means further comprises gravity compensating means for eliminating the effect of acceleration due to gravity from the detected acceleration.

14. A coordinate input device according to claim 11;

wherein the first coordinate system is a dynamic system comprising at least two coordinate axes wherein the second coordinate system is a static system comprising at least two axes wherein the origin is a static, predetermined point.

15. A coordinate input device according to claim 11;

further comprising second coordinate conversion means for converting the coordinates of the coordinate indicator in the second coordinate system into the coordinates at the tip of the coordinate indicator in the second coordinate system.

16. A coordinate input device according to claim 11;

wherein the attitude detecting means comprises angular acceleration detecting means for detecting an angular acceleration of the coordinate indicator, second integrating means for converting the angular acceleration into angular velocity or angular information, and direction operation means for converting the angular velocity or angular information into the attitude of the coordinate indicator.

17. A coordinate input device according to claim 16;

wherein the direction operation means includes means for performing coordinate transformation of the spatial coordinates of the coordinate indicator in accordance with a 3×

3 matrix A_ij coefficient representing three dimensional rotation defined by the following equation;

##EQU11## wherein the matrix coefficients A_ij, (i=1-3, j=1-3), represent the attitude of the coordinate indicator, PX, PY and PZ represent coordinates in the first coordinate system and SX, SY and SZ represent coordinates in the second coordinate system.

18. A coordinate input device according to claim 17;

wherein the direction operation means includes means for calculating A_ij at time intervals of delta t, and wherein the relationship between the matrix A_ij and the angular velocity or angular information of the coordinate indicator is defined by the following equations;

space="preserve" listing-type="equation">A.sub.ij (t)=A.sub.ij (t-delta t)·

W.sub.ij (t)

space="preserve" listing-type="equation">W11(t)=W22(t)=W33(t)=1

space="preserve" listing-type="equation">W23(t)=-W32(t)=delta t·

WX(t)

space="preserve" listing-type="equation">W31(t)=-W13(t)=delta t·

WY(t)

space="preserve" listing-type="equation">W12(t)=-W21(t)=delta t·

WZ(t)

wherein (delta t) represents a calculation period of the device, A_ij (t) is a three dimensional matrix representing the attitude of the coordinate indicator, and W_ij (t) represents the angular velocity or angular information of the coordinate indicator.

19. A coordinate input device according to claim 11;

wherein the attitude detecting means comprises angular velocity detecting means for detecting an angular velocity of the coordinate indicator, direction operation means for determining the attitude of the coordinate indicator using the output from the angular velocity detecting means, acceleration detecting means for detecting the acceleration of the coordinate indicator, coordinate converting means for performing coordinate transformation of a detected acceleration of the coordinate indicator using the output from the direction operation means, gravity compensation means for removing an effect of gravity from the detected acceleration of the coordinate indicator, and filter means for removing a dynamic component from the detected acceleration of the coordinate indicator.

20. A coordinate input device according to claim 11;

wherein the coordinate detecting means comprises an acceleration detecting means fixed in the coordinate indicator for detecting an acceleration of the coordinate indicator, first integrating means for integrating the acceleration output by the acceleration detecting means and for determining the velocity of the coordinate indicator, second integrating means for integrating the velocity output by the first integrating means and for determining the position of the coordinate indicator, and negative feedback means for performing negative feedback from the output of the second integrating means to the input of said first integrating means.

21. A coordinate input device according to claim 11;

wherein the coordinate detecting means comprises an acceleration detecting means fixed in the coordinate indicator for detecting an acceleration of the coordinate indicator, first integrating means for integrating the acceleration output by the acceleration detecting means and for determining the velocity of the coordinate indicator, second integrating means for integrating the velocity output of the first integrating means and for determining the position of the coordinate indicator, and at least one of a negative feedback means for performing negative feedback from the output of the first integrating means to the input of the first integrating means or a negative feedback means for performing negative feedback from the output of the second integrating means to the input of the second integrating means.

22. A method for calculating the spatial coordinates at the tip of a coordinate indicator, comprising the steps of:

(a) detecting the acceleration at a detecting point of a coordinate indicator in at least two dimensions in a first coordinate system;

(b) determining the attitude of the coordinate indicator;

(c) transforming the acceleration of the detecting point in the first coordinate system to a second coordinate system which is a static coordinate system having a predetermined origin, the transformation being performed in accordance with the attitude of the coordinate indicator;

(d) subtracting the acceleration due to gravity from the transformed detected acceleration value;

(e) integrating the transformed detected acceleration to obtain the spatial coordinates of the detecting point; and

(f) determining the spatial coordinates at the tip of the coordinate indicator in accordance with the spatial coordinates at the detecting point and the attitude of the coordinate indicator.

23. A method according to claim 22;

wherein the attitude of the coordinate indicator is determined by detecting the angular acceleration of the coordinate indicator, integrating the angular acceleration to convert it into angular velocity or angular information of the coordinate indicator, and determining the attitude of the coordinate indicator using the angular velocity or angular information.

24. A method according to claim 23;

wherein the attitude is determined in accordance with the following equation;

space="preserve" listing-type="equation">A.sub.ij (t)=A.sub.ij (t-delta t)·

W.sub.ij (t)

space="preserve" listing-type="equation">W11(t)=W22(t)=W33(t)=1

space="preserve" listing-type="equation">W23(t)=-W32(t)=delta t·

WX(t)

space="preserve" listing-type="equation">W31(t)=-W13(t)=delta t·

WY(t)

space="preserve" listing-type="equation">W12(t)=-W21(t)=delta t·

WZ(t)

wherein (delta t) represents a calculation period, A_ij (t) is a three-dimensional matrix representing the attitude of the coordinate indicator, and W_ij (t) represents the angular velocity or angular information of the coordinate indicator.

25. A method according to claim 22;

wherein the attitude of the coordinate indicator is determined by detecting acceleration at three points within the coordinate indicator, said three points not being on the same line, integrating the acceleration values to determine spatial coordinates at each point, and obtaining the difference between the coordinates at the three points to determine the attitude of the coordinate indicator.

26. A coordinate input device for obtaining the spatial coordinates of a pen-type coordinate indicator, comprising:

acceleration detecting means for detecting the acceleration of a body of the pen-type coordinate indicator and producing an output;

attitude detecting means for detecting the attitude of the body of the pen-type coordinate indicator with respect to a tip thereof and producing an output; and

coordinate operation means for determining the spatial coordinates at the tip of the coordinate indicator in accordance with the outputs of the acceleration detecting means and the attitude detecting means such that movement of the body of the coordinate indicator alone is not erroneously detected as movement of the tip.

27. A coordinate input device for calculating the spatial coordinates at the tip of a pen-type coordinate indicator, the coordinate input device comprising:

coordinate detecting means for determining the spatial coordinates of a pen-type coordinate indicator in a first coordinate system;

attitude detecting means for determining the attitude of a body of the coordinate indicator with respect to a tip thereof; and

first coordinate conversion means for determining the spatial coordinates at the tip of the coordinate indicator in a second coordinate system in accordance with the spatial coordinates of the coordinate indicator body in the first coordinate system and the attitude of the coordinate body such that movement of the body of the coordinate indicator alone is not erroneously detected as movement of the tip.

28. A coordinate input device for obtaining the spatial coordinates at the tip of a pen-type coordinate indicator, comprising:

acceleration detecting means for detecting the acceleration of a body of the pen-type coordinate indicator and producing an output;

attitude detecting means for detecting the attitude of the body of the pen-type coordinate indicator and producing an output; and

coordinate operation means for determining the spatial coordinates at the tip of the coordinate indicator in accordance with the outputs of the acceleration detecting means and the attitude detecting means and predetermined data indicating the relationship between the positions of the acceleration detecting means and the tip of the coordinate indicator.