Increasing cursor control device sensitivity
An aircraft includes a cursor control device having a defined return path for the touch sensor so that the impedance in the return path is known. The defined return path is embodied in a conductive feature in the cursor control device palm contact area to ground the user and improve the system's signal to noise ratio. The defined return path normalizes signal variability due to environmental factors and user specific factors such as finger size, skin moisture, contaminants, etc.
1. A cursor control device comprising:
a capacitive touch screen;
a signal generator connected to the capacitive touch screen; and
a return path contact connected to a ground terminal of the signal generator,
wherein the return path contact comprises a plurality of posts disposed in a palm rest portion, each of the plurality of posts, each comprising a threaded shaft and hemispherical portion, the threaded shaft configured to screw into the palm rest portion and contact a ground, the hemispherical portions protruding from the palm rest portion to contact a portion of a user's hand configured to reduce impedance in a signal path.
2. The cursor control device of claim 1 , wherein the return path contact comprises at least one metallic plate embedded in the palm rest portion.
3. The cursor control device of claim 2 , wherein the at least one metallic plate protrudes above a surface of the palm rest portion.
4. The cursor control device of claim 1 , wherein the return path contact comprises a conductive paint applied to the palm rest portion.
5. The cursor control device of claim 1 , wherein the return path contact comprises a conductive front plate.
6. The cursor control device of claim 1 , wherein the return path contact produces a return path impedance of less than 20 k ohms.
7. A computer apparatus comprising:
a capacitive touch screen;
a signal generator connected to the capacitive touch screen; and
a return path contact connected to a ground terminal of the signal generator,
wherein the return path contact comprises a plurality of posts disposed in a palm rest portion, each of the plurality of posts, each comprising a threaded shaft and hemispherical portion, the threaded shaft configured to screw into the palm rest portion and contact a ground, the hemispherical portions protruding from the palm rest portion to contact a portion of a user's hand configured to reduce impedance in a signal path.
8. The computer apparatus of claim 7 , wherein the return path contact comprises at least one metallic plate embedded in the palm rest portion.
9. The computer apparatus of claim 8 , wherein the at least one metallic plate protrudes above a surface of the palm rest portion.
10. The computer apparatus of claim 7 , wherein the return path contact comprises a conductive paint applied to the palm rest portion.
11. The computer apparatus of claim 7 , wherein the return path contact produces a return path impedance of less than 20 k ohms.
12. An aircraft comprising:
a cursor control device comprising:
a capacitive touch screen;
a signal generator connected to the capacitive touch screen; and
a return path contact connected to a ground terminal of the signal generator,
wherein the return path contact comprises a plurality of posts disposed in a palm rest portion, each of the plurality of posts, each comprising a threaded shaft and hemispherical portion, the threaded shaft configured to screw into the palm rest portion and contact a ground, the hemispherical portions protruding from the palm rest portion to contact a portion of a user's hand to reduce impedance in a signal path at the capacitive touch screen.
13. The aircraft of claim 12 , wherein the return path contact comprises at least one metallic plate embedded in the palm rest portion.
14. The aircraft of claim 13 , wherein the at least one metallic plate protrudes above a surface of the palm rest portion.
15. The aircraft of claim 12 , wherein the return path contact comprises a conductive paint applied to the palm rest portion.
16. The aircraft of claim 12 , wherein the return path contact comprises a conductive front plate.
17. The aircraft of claim 12 , wherein the return path contact produces a return path impedance of less than 20 k ohms.