System and method for separating attached field emission structures
An improved field emission system and method is provided that involves field emission structures having electric or magnetic field sources. The magnitudes, polarities, and positions of the magnetic or electric field sources are configured to have desirable correlation properties, which may be in accordance with a code. The correlation properties correspond to a desired spatial force function where spatial forces between field emission structures correspond to relative alignment, separation distance, and the spatial force function.
1. A method for separating attached field emission structures, comprising the steps of:
maintaining a position of a first field emission structure that is attached to a second field emission structure, each one of a plurality of field emission sources of said first field emission structure being substantially aligned with a corresponding one of a plurality of field emission sources of said second field emission structure thereby producing a peak spatial force in accordance with a spatial force function; and
moving said second field emission structure relative to said first field emission structure such that each one of said plurality of field emission sources of said first field emission structure becomes unaligned with a corresponding one of said plurality of field emission sources of said second field emission structure, said spatial force function being in accordance with a code, said code corresponding to a code modulo of said plurality of field emission sources of said first field emission structure and a complementary code modulo of said plurality of field emission sources of said second field emission structure, said code defining said peak spatial force corresponding to substantial alignment of said code modulo of said plurality of field emission sources of said first field emission structure with said complementary code modulo of said plurality of field emission sources of said second field emission structure, said code also defining a plurality of off peak spatial forces corresponding to a plurality of different misalignments of said code modulo of said plurality of field emission sources of said first field emission structure and said complementary code modulo of said plurality of field emission sources of said second field emission structure, said plurality of off peak spatial forces having a largest off peak spatial force, said largest off peak spatial force being less than half of said peak spatial force.
2. The method of claim 1 , wherein said moving said second field emission structure relative to said first field emission structure is in accordance with one of a one-dimensional movement path function, a two-dimensional movement path function, or a three-dimensional movement path function.
3. The method of claim 1 , wherein said moving said second field emission structure relative to said first field emission structure is in accordance with at least one of a linear movement path function, a non-linear movement path function, a rotational movement path function, a cylindrical movement path function, or a spherical movement path function.
4. The method of claim 1 , wherein said moving said second field emission structure relative to said first field emission structure corresponds to a at least one of a forward movement, a backward movement, an upward movement, a downward movement, a left movement, a right movement, a yaw, a pitch, and or a roll.
5. The method of claim 1 , wherein said moving said second field emission structure relative to said first field emission structure is in accordance with a movement vector having a direction and amplitude that varies over time.
6. The method of claim 1 , wherein said moving said second field emission structure relative to said first field emission structure is accomplished using one of a turning mechanism, a lever, or a tool.
7. The method of claim 1 , further comprising the step of:
unlatching a latching mechanism prior to moving said second field emission structure relative to said first field emission structure.
8. The method of claim 1 , wherein said first field emission structure is associated with a first object.
9. The method of claim 8 , wherein said second field emission structure is associated with a second object.
10. A system for separating attached field emission structures, comprising:
a first mechanism that maintains a position of a first field emission structure that is attached to a second field emission structure, each one of a plurality of field emission sources of said first field emission structure being substantially aligned with a corresponding one of a plurality of field emission sources of said second field emission structure thereby producing a peak spatial force in accordance with a spatial force function; and
a second mechanism that moves said second field emission structure relative to said first field emission structure such that each one of said plurality of field emission sources of said first field emission structure becomes unaligned with a corresponding one of said plurality of field emission sources of said second field emission structure, said spatial force function being in accordance with a code, said code corresponding to a code modulo of said plurality of field emission sources of said first field emission structure and a complementary code modulo of said plurality of field emission sources of said second field emission structure, said code defining said peak spatial force corresponding to substantial alignment of said code modulo of said plurality of field emission sources of said first field emission structure with said complementary code modulo of said plurality of field emission sources of said second field emission structure, said code also defining a plurality of off peak spatial forces corresponding to a plurality of different misalignments of said code modulo of said plurality of field emission sources of said first field emission structure and said complementary code modulo of said plurality of field emission sources of said second field emission structure, said plurality of off peak spatial forces having a largest off peak spatial force, said largest off peak spatial force being less than half of said peak spatial force.
11. The system of claim 10 , wherein said second mechanism moves said second field emission structure relative to said first field emission structure in accordance with one of a one-dimensional movement path function, a two-dimensional movement path function, or a three-dimensional movement path function.
12. The system of claim 10 , wherein said second mechanism moves said second field emission structure relative to said first field emission structure in accordance with at least one of a linear movement path function, a non-linear movement path function, a rotational movement path function, a cylindrical movement path function, or a spherical movement path function.
13. The system of claim 10 , wherein said second mechanism moves said second field emission structure relative to said first field emission structure using at least one of a forward movement, a backward movement, an upward movement, a downward movement, a left movement, a right movement, a yaw, a pitch, and or a roll.
14. The system of claim 10 , wherein said second mechanism moves said second field emission structure relative to said first field emission structure in accordance with a movement vector having a direction and amplitude that varies over time.
15. The system of claim 10 , wherein said second mechanism comprises one of a turning mechanism, a lever, or a tool.
16. The system of claim 10 , further comprising:
a latching mechanism.
17. The system of claim 10 , wherein said first field emission structure is associated with a first object.
18. The system of claim 17 , wherein said second field emission structure is associated with a second object.