1460706968-9abf27f9-72a2-45b7-ac73-7e2bc4d33166

1. A packaged searching system, comprising:
a memory configured to store program instructions; and
a processor configured to execute the program instructions, the program instructions when executed configured to:
display search target objects selected on a map to distinguish the search target objects from unselected objects;
create and display search boxes on the map, wherein each of the search boxes correspond to the respective distinguished search target objects;
map the distinguished search target objects to the created search boxes;
search information regarding the search target objects mapped to the respective search boxes using input search keywords; and
display the searched information for each search target object.
2. The packaged searching system according to claim 1, wherein the program instructions when executed am further configured to display the search boxes on the map to locate each of the search boxes on the respective search target objects.
3. The packaged searching system according to claim 1, wherein the program instructions when executed are further configured to create the search boxes in a layer different from a layer in which map information is displayed.
4. The packaged searching system according to claim 1, wherein the program instructions when executed are further configured to search for relation information between the search target objects with the searched information.
5. The packaged scanting system according to claim 4, wherein the program instructions when executed are further configured to display the relation information on a search result display box for each search target object.
6. The packaged searching system according to claim 1, wherein the program instructions when executed are further configured to map the search boxes to search target objects by assigning a value of each search box object to member variables of the respective objects to base each of the search box objects on the respective search target objects.
7. The packaged searching system according to claim 1, wherein the program instructions when executed are further configured to map the search boxes to the search target objects by invoking a method between the search target objects or the search box objects to transmit identifier information.
8. The packaged searching system according to claim 1, wherein the program instructions when executed are further configured to map the search boxes to the search target objects by invoking an interface disposed between layers to transmit identifier information, when the search target objects and the search box objects are configured as layers.
9. The packaged searching system according to claim 1, wherein the search target objects are space of interest (SOI) objects displayed on a SOI map.
10. A packaged searching system, comprising:
a memory configured to store program instructions; and
a processor configured to execute the program instructions, the program instructions when executed configured to:
create search boxes to define at least one search target object;
display a plurality of search target objects moved into the search boxes to distinguish the search target objects;
map the search target objects in the search box to corresponding search boxes;
a search for information regarding the at least one search target object in the corresponding search box using search keywords input in the search boxes; and
display on a screen the searched information for the at least one search target object.
11. The packaged searching system according to claim 10, wherein the program instructions when executed are further configured to create the search boxes as a bucket that includes a keyword input box in which a search keyword is input and an area in which the search target objects are dropped.
12. The packaged searching system according to claim 11, wherein the program instructions when executed are further configured to creates search boxes wherein different space of interest (SOI) objects correspond to different search keywords.
13. The packaged searching system according to claim 11, wherein the search box includes a list from which lower-level space of interest objects may be selected when the search target objects include lower-level space of interest objects.
14. The packaged searching system according to claim 11, wherein the program instructions when executed are further configured to display the searched information as a bucket for each search target object or display the search target objects and searching information regarding the search target objects as a list.
15. The packaged searching system according 14, wherein the program instructions when executed are further configured to display a number of search results for each search target object on the corresponding search target object on the map.
16. The packaged searching system according to claim 14, wherein the program instructions when executed are further configured to display the information regarding the search target object in the selected bucket on the search area when one of the buckets displayed on a search area is selected.
17. The packaged searching system according to claim 16, wherein the program instructions when executed are further configured to display the search target object with the information to distinguish turn other search target objects on the map.
18. The packaged searching system according to claim 11, wherein the program instructions when executed are further configured to display buckets that correspond to the search target objects as being stacked and display a number that indicates how many buckets are stacked when a plurality of search target objects are searched for with a same search keyword.
19. The packaged searching system according to claim 10, wherein the program instructions when executed are further configured to display recommendation information on a map based on user preference when recommendation information is detected for the search target objects.
20. The packaged searching system according to claim 10, wherein the program instructions when executed are further configured to determine dropped search target objects as selected search target objects when the search target objects are dragged and dropped in one of the search boxes.
21. The packaged searching system according to claim 10, wherein the program instructions when executed are further configured to perform packaged searching for information regarding the plurality of search target objects with a same search keyword input in the search box when a plurality of search target objects are included in a same search box.
22. The packaged searching system according to claim 10, wherein the program instructions when executed are further configured to perform packaged searching for information regarding the plurality of search target objects with search keywords each input in the respective search boxes when a plurality of search target objects are included in a plurality of search boxes.
23. The packaged searching system according to claim 22, wherein the program instructions when executed are further configured to search for relation information between the search target objects in the search boxes.
24. The packaged searching system according to claim 10, wherein the program instructions when executed are further configured to search for information regarding lower-level objects when the search target objects include lower-level objects.
25. The packaged searching system according to claim 10, wherein the search target objects are space of interest (SOI) objects displayed on a SOI map.
26. A packaged searching method, comprising
selecting, by a processor, searching target objects on a map;
creating, by the processor, a search box for each selected search target object to display the search box on the map;
performing, by the processor, packaged searching for information regarding the search target objects using a search keyword input in the search box; and
displaying, by the processor, searched information for each selected search target on the map.
27. The packaged searching method according to claim 26, wherein performing the packaged searching includes searching, by the processor, relation information between the search target objects.
28. The packaged searching method according to claim 26, wherein performing the packaged searching includes searching, by the processor, information regarding lower-level objects when the search target objects include lower-level objects.
29. The packaged searching method according to claim 26, wherein the search target objects are space of interest (SOI) objects displayed on a SOI map.
30. A packaged searching method, comprising;
creating, by a processor, search boxes to define search target objects;
defining, by the processor, search target objects by selecting objects on a map to move the selected objects to the search boxes;
searching, by the processor, for information regarding the defined search target objects with search keywords input in the search boxes; and
displaying, by the processor, the searched information.
31. The packaged searching system according to claim 30, wherein searching for the information includes performing, by the processor, packaged searching for information regarding the defined search target objects with a same search keyword input in the search box when a plurality of search target objects are included in a same search box.
32. The packaged searching system according to claim 30, wherein searching for the information includes performing, by the processor, packaged searching for the search target objects moved into the search boxes with search keywords each input in the respective search boxes when a plurality of search boxes are created and at least one search target object is included in each of the search boxes.
33. The packaged searching system according to claim 30, wherein the search target objects are space of interest (SOI) objects displayed on an SOI map.
34. A non-transitory computer readable medium containing program instructions executed by a processor, the computer readable medium comprising:
program instructions that select searching target objects on a map;
program instructions that create a search box for each selected search target object to display the search box on the map;
program instructions that perform packaged searching for information rewarding the search target objects using a search keyword input in the search box; and
program instructions that display searched information for each selected search target on the map.
35. The non-transitory computer readable medium of claim 34, wherein performing the packaged searching includes program instructions that search relation information between the search target objects.
36. The non-transitory computer readable medium of claim 34, wherein performing the packaged searching includes program instructions that search information regarding lower-level objects when the search target objects include lower-level objects.
37. A non-transitory computer readable medium containing program instructions executed by a processor, the computer readable medium comprising:
program instructions that create search boxes to define search target objects;
program instructions that define search target objects by selecting objects on a map to move the selected objects to the search boxes;
program instructions that search for information regarding the defined search target objects with search keywords input in the search boxes; and
program instructions that display the searched information.
38. The non-transitory computer readable medium of claim 37, wherein the search target objects are space of interest (SOI) objects displayed on an SOI map.

The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.

1. A bottom antireflective coating for photolithography using wavelengths of 157 nm or less, comprising a crosslinkable polymer which includes cinnamic acid derivatives.
2. The bottom antireflective coating of claim 1, wherein cinnamic acid derivatives are contained either in the polymer backbone or in side chains of the polymer.
3. The bottom antireflective coating of claim 1, wherein the bottom antireflective coating contains a polymer of one of the following formulas I-III:
wherein:
R1 comprises H, halogen, and a straight or branched alkyl chain including 1-10 C atoms;
R2 comprises one or more substituents at one or more of the 1, 2, 3, 4 and 5 positions on the phenyl ring, the one or more substituents being independent of each other and each substituent comprising at least one of H, a straight or branched alkyl chain including 1-4 C atoms, a halogen, NO2, NH2 or OH;
R3 is one of the following:
or another group comprising polymer units that are polymerizable with each other;
m is an integer of 1-10,000;
n is 0 or an integer of 1-10,000;
o and p are independent of each other and each is an integer of 1-10;
R4 comprises a carboxyl protective group, a straight or branched alkyl group including 1-4 C atoms, or a group cleavable by a nucleophilic reagent or acid; and
X comprises a reactive anchor group.
4. The bottom antireflective coating of claim 1, wherein the polymer is a copolymer between the cinnamic ester monomers and a monomer including an anchor group.
5. The bottom antireflective coating of claim 3, wherein the reactive anchor group (X) is selected from the group consisting of acid anhydride, epoxide and ketene.
6. The bottom antireflective coating of claim 5, wherein the reactive anchor group (X) is an acid anhydride group.
7. The bottom antireflective coating of claim 6, wherein the acid anhydride group is derived from maleic anhydride, itaconic anhydride, methacrylic anhydride, cyclohexenedicarboxylic anhydride or norbornenedicarboxylic anhydride.
8. The bottom antireflective coating of claim 7, wherein the acid anhydride group is derived from maleic anhydride.
9. The bottom antireflective coating of claim 8, wherein the polymer has a structure according to the following formula V:
wherein R1, R2, R4, m and n are as described above for formulas (I-III).
10. The bottom antireflective coating of claim 9, wherein the polymer has a structure of the following formula VI:
wherein R1, R2, m and n are as defined for formulas (I-III).
11. The bottom antireflective coating of claim 5, wherein a molar proportion of a second repeating unit of the polymer is in a range from 10 to 50 mol %.
12. The bottom antireflective coating of claim 1, wherein the polymer is crosslinked.
13. The bottom antireflective coating of claim 12, wherein the crosslinking is achieved photochemically.
14. The bottom antireflective coating of claim 12, wherein the crosslinking is achieved utilizing a wet chemical method.
15. The bottom antireflective coating of claim 14, wherein the crosslinking is achieved using a bisalkylamine, a bisisocyanate or a bisalcohol.
16. A formulation for the production of a bottom antireflective coating for photolithography using wavelengths of not more than 157 nm, comprising the polymer of claim 1, a solvent and a stabilizer.
17. The formulation of claim 16, comprising a protected, bifunctional crosslinking agent.
18. The formulation of claim 15, wherein the protected, bifunctional crosslinking agent is selected from the group consisting of thermally labile bisamines and bifunctional thermo acids.
19. A process for the production of a bottom antireflective coating, comprising the following steps:
applying the formulation of claim 16 to a substrate by spin coating;
evaporating the solvent in a post apply bake (PAB) step; and
crosslinking the polymer contained in the formulation.
20. A process for conducting photolithography using wavelengths of 157 nm or less, comprising the step of using the polymer of claim I for the production of a bottom antireflective coating for the photolithography process.

1460706965-3fc07cdb-3402-4cc1-8a68-1d553d228435

1. An apparatus comprising:
a first strut having a first end and a second end opposite the first end, the first end of the first strut operatively coupled to a fuselage of an aircraft and the second end of the first strut operatively coupled to a wing of the aircraft; and
a first actuator operatively coupled to the first strut to change an effective length of the first strut.
2. The apparatus of claim 1, wherein the first actuator is operatively coupled between the first end of the first strut and the fuselage of the aircraft.
3. The apparatus of claim 2 further comprising a second strut having a first end and a second end opposite the first end, the first end of the second strut operatively coupled to the fuselage of the aircraft and the second end of the second strut operatively coupled to the wing of the aircraft.
4. The apparatus of claim 3 further comprising a second actuator operatively coupled between the first end of the second strut and the fuselage to change an effective length of the second strut.
5. The apparatus of claim 4, wherein the second end of the first strut is operatively coupled to the wing proximate a forward spar in the wing and the second end of the second strut is operatively coupled to the wing proximate an aft spar in the wing.
6. The apparatus of claim 1 further comprising a controller to operate the actuator to change the effective length of the first strut based on at least one of an altitude of the aircraft, a speed of the aircraft, a weight of the wing of the aircraft, or a change in shape of the wing during flight.
7. The apparatus of claim 6 further comprising a sensor operatively coupled to the wing to detect the change in shape of the wing during flight.
8. The apparatus of claim 1, wherein the first actuator comprises a shape memory alloy wire.
9. An apparatus comprising:
a first strut operatively coupled between a fuselage of an aircraft and a wing of the aircraft to support the wing during flight; and
a first actuator to adjust a tension in the first strut during flight.
10. The apparatus of claim 9 further comprising a sensor to detect twist in the wing, wherein the first actuator is to adjust the tension in the first strut during flight based on the twist.
11. The apparatus of claim 9, wherein the first strut is operatively coupled to a forward spar in the wing.
12. The apparatus of claim 11 further comprising a second strut operatively coupled between the fuselage and the wing to support the wing during flight, the second strut operatively coupled to an aft spar in the wing.
13. The apparatus of claim 12 further comprising a second actuator to adjust a tension in the second strut during flight.
14. A method comprising:
measuring a deflection of a wing of an aircraft during flight, the aircraft having a first strut coupled between the wing and a fuselage of the aircraft; and
adjusting an effective length of the first strut between the wing and the fuselage based on the measured deflection of the wing to change the deflection of the wing.
15. The method of claim 14, wherein the aircraft includes a second strut coupled between the wing and the fuselage.
16. The method of claim 15 further comprising adjusting an effective length of the second strut between the wing and the fuselage based on the measured deflection of the wing to change the deflection of the wing.
17. The method of claim 16, wherein the first strut is coupled to a forward spar in the wing and the second strut is coupled to an aft spar in the wing.
18. The method of claim 16, wherein adjusting the effective length of the first strut comprises extending the first strut to increase the effective length of the first strut and adjusting the effective length of the second strut comprises shortening the second strut to decrease the effective length of the second strut.
19. The method of claim 14, wherein the deflection of the wing is measured via a sensor operatively coupled to the wing.
20. The method of claim 19 further comprising:
determining at least one of an altitude of the aircraft, a speed of the aircraft, or a volume of fuel in the wing; and
adjusting the effective length of the first strut based on the least one of the determined altitude, speed, or volume.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.

1. An ozone generation system comprising:
an ozone generator adapted to deliver a given amount of ozone in a space in order to obtain a target concentration therein;
a variable direct current power supply connected to the ozone generator and having a first input for receiving an alternating current power signal and a second input for an external control signal;
a control unit connected to the second input of the power supply for generating the external control signal, the external control signal being generated in accordance with an amount of ozone required in order to reach the target concentration; and
an ozone sensor connected to the control unit and adapted to measure a residual amount of ozone in the space and provide the control unit with a measurement signal of the residual amount for determining the amount of ozone required.
2. The ozone generation system of claim 1, wherein the power supply is controllable from substantially 0% to substantially 100% of an available output voltage.
3. The ozone generation system of claim 1, wherein the power supply comprises a solid-state relay connected to an input of a rectifier, for metering an amount of the alternating current power signal presented to the rectifier, and a filter connected to an output of the rectifier for smoothing out a rectified signal and presenting the rectified signal to the ozone generator.
4. The ozone generation system of claim 1, wherein the filter is one of an inductor-capacitor filter and a capacitor-inductor-capacitor filter.
5. (canceled)
6. The ozone generation system of claim 1, wherein the external control signal is one of an alternating current signal from about 4 ma to about 20 ma and a direct current signal from about 0 volts to about 10 volts.
7. (canceled)
8. The ozone generation system of claim 1, wherein the rectifier is a full-wave rectifier.
9. The ozone generation system of claim 1, wherein the control unit comprises a Proportional-Integral-Derivative (PID) controller.
10. The ozone generation system of claim 1, wherein the control unit comprises a control device to vary a corona frequency and a corona voltage, a control loop feedback mechanism, and an interface for setting control parameters.
11. The ozone generation system of claim 10, wherein the control unit is adapted for setting the control parameters remotely.
12. The ozone generation system of claim 1, wherein the ozone generator comprises at least one output valve for selectively outputting generated ozone into the space and at least one dump valve for disposing of ozone when the at least one output valve is closed.
13. The ozone generation system of claim 12, wherein the at least one output valve is a proportional control valve controlled by the control unit.
14. The ozone generation system of claim 12, wherein each one of the at least one output valve is associated with a given zone in the space, and is controlled in accordance with ozone to be delivered to the given zone.
15. The ozone generation system claim 12, wherein the ozone generator comprises a flow sensor for measuring a flow rate of clean air provided to an ozone generating tube inside the ozone generator, and the flow rate as measured is provided to the control unit.
16. The ozone generation system of claim 15, wherein the flow sensor is an electronic flow sensor provided upstream from the ozone generating tube, in an input path thereof.
17. A method for generating ozone in a space, the method comprising:
measuring a concentration of residual ozone in the space;
determining, from the concentration measured, an amount of ozone required for providing a target concentration of ozone in the space;
generating an external control signal for energizing a variable direct current power supply, the external control signal having a value selected in accordance with the amount of ozone required;
energizing the variable direct current power supply with the external control signal and supplying the direct current power supply with an alternating current power signal;
metering an amount of the alternating current power signal allowed to flow through the variable direct current power supply by varying a conduction angle thereof, thereby causing the variable direct current power supply to output a predetermined voltage level to an ozone generator; and
delivering the amount of ozone required for providing the target concentration in the space.
18. The method of claim 17, wherein metering an amount of the alternating current power signal comprises metering from substantially 0% to substantially 100% of the alternating current power signal.
19. The method of claim 17, wherein metering an amount of the alternating current power signal comprises chopping the alternating current power signal using a solid state relay, rectifying a chopped signal, and filtering a rectified signal to provide the predetermined voltage level to the ozone generator.
20. The method of claim 17, wherein energizing the variable direct current power supply comprises providing the variable direct current power supply with one of an alternating current control signal from about 4 ma to about 20 ma and a direct current control signal from about 0 volts to about 10 volts.
21. (canceled)
22. The method of claim 17, wherein energizing the variable direct current power supply comprises energizing upon a zero-crossing of the alternating current power signal.
23. The method of claim 17, wherein causing the variable direct current power supply to output a predetermined voltage level comprises outputting a predetermined voltage level that is substantially linear with respect to the external control signal.
24. (canceled)
25. (canceled)
26. The method of claim 17, wherein delivering the amount of ozone comprises selectively opening and closing at least one output valve, and selectively opening at least one dump valve when the at least one output valve is closed.
27. (canceled)
28. The method of claim 26, wherein delivering the amount of ozone comprises selectively delivering the ozone to at least two zones of the space, each one of the at least two zones having at least one of the at least one output valve assigned thereto.
29. The method of claim 26, further comprising measuring a flow rate of a clean air input, and using the flow rate as measured to dynamically open and close the at least one output valve and the at least one dump valve.
30. A fully variable direct current power supply having a first input for receiving an alternating current power signal and a second input for an external control signal, the power supply comprising a solid-state relay and a rectifier, the solid state relay, connected to an input of the rectifier, adapted for metering the alternating current power signal presented to the rectifier from substantially 0% to substantially 100%, and a filter connected to an output of the rectifier for smoothing out a rectified signal and outputting a direct current voltage signal.
31. A method for generating a direct current voltage signal, the method comprising energizing the variable direct current power supply with an external control signal and an alternating current power signal, metering from substantially 0% to substantially 100% an amount of the alternating current power signal allowed to flow through the variable direct current power supply as a function of the external control signal by varying a conduction angle thereof using a solid state relay, rectifying an output of the solid state relay, filtering a rectified signal, and outputting a direct current voltage signal.