CN106767180A - Flight formula throwing device, throwing Target process and system - Google Patents
Flight formula throwing device, throwing Target process and system Download PDFInfo
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- CN106767180A CN106767180A CN201710002249.XA CN201710002249A CN106767180A CN 106767180 A CN106767180 A CN 106767180A CN 201710002249 A CN201710002249 A CN 201710002249A CN 106767180 A CN106767180 A CN 106767180A
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- 238000000034 method Methods 0.000 title claims abstract description 27
- 238000001514 detection method Methods 0.000 claims description 32
- 238000003384 imaging method Methods 0.000 claims description 12
- 238000001093 holography Methods 0.000 claims description 2
- 239000011800 void material Substances 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
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- 238000006243 chemical reaction Methods 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J9/00—Moving targets, i.e. moving when fired at
- F41J9/08—Airborne targets, e.g. drones, kites, balloons
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/12—Target-seeking control
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- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
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- Physics & Mathematics (AREA)
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- Automation & Control Theory (AREA)
- General Engineering & Computer Science (AREA)
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Abstract
The present invention provides a kind of flight formula throwing device, throws Target process and system, belongs to throwing target field.The flight formula throwing device includes：Flying unit and throwing target unit, the flying unit carry the throwing target unit flight, and the target unit of throwing is used to according to the instruction release target body for receiving.Flight formula throwing device may be implemented in flight course and carry out throwing target using throwing target unit, to realize mobile throwing target, difference according to flying height casts out the target body of different angles, to meet the demand of user, and flight formula throwing device may move and be easy to carry, expand and use scope, motion is shot in ad-hoc location without user.
Description
Technical field
The present invention relates to throw target field.
Background technology
The position of existing trap machine is fixed, it is impossible to realize it is mobile throw target, user in shooting, because the track for throwing target is consolidated
Fixed, shooting difficulty is low.Cannot realize that multi-angle casts, it is impossible to meet the requirement of user.
The content of the invention
Present invention offer is a kind of to be intended to that the flight formula throwing device of target can be thrown in flight, throws Target process and system.
Concrete technical scheme is as follows：
A kind of flight formula throwing device, the device includes：Flying unit and throwing target unit, the flying unit carries described
The flight of target unit is thrown, the target unit of throwing is to according to the instruction release target body for receiving.
Preferably, the flying unit uses rotary wind type flight structure, or
The flying unit uses flapping wings type flight structure, or
The flying unit uses fixed-wing formula flight structure, or
The flying unit uses umbrella wing formula flight structure, or
The flying unit uses jet-propelled flight structure, or
The flying unit uses dirigible structure.
Preferably, the target body includes entity target body, and/or virtual target body.
Preferably, the entity target body uses plate shape structure, loop configuration or rectangular configuration, or
The entity target body is the balloon of filling gas, or
The entity target body is the target body for being provided with light source.
Preferably, the virtual target body is the virtual target body presented using optics.
Preferably, the virtual target body is that the virtual target body is presented using holographic imaging mode.
Preferably, it is described throwing target unit include,
First receiver module, is used to receive control instruction；
Storage target cabin, is used to store the entity target body；
Ejection portion, is used to for the outlet of the entity target body from the throwing target unit to launch output；
First detection module, is used to detect the position data of the throwing target unit；
First control module, connects first receiver module, the ejection portion and the first detection module respectively, uses
Controlled described in the ejection portion ejection with the position data detected according to the first detection module and the control instruction
Entity target body.
Preferably, it is described throwing target unit include,
Second receiver module, is used to receive control instruction；
Emission part, is used to using holographic imaging mode output light, so that the virtual target body is presented；
Second detection module, is used to detect the position data of the throwing target unit, the position data include altitude information,
Air speed data and coordinate data；
Second control module, connects second receiver module, the emission part and second detection module respectively, uses
The emission part is controlled to be imaged with the position data detected according to second detection module and the control instruction.
Preferably, the flying unit includes,
Locating module, is used to position the positional information of the flying unit；
3rd receiver module, is used to receive flight directive；
Flight module, connects the locating module and the 3rd receiver module, to according to the flight directive respectively
And the positional information flight, or
The flight module is used to be flown to target location according to the flight directive and the positional information.
The present invention also provides a kind of flight formula and throws Target process, including the step of be：
Flying unit carries throwing target unit and is flown；
It is described to throw the target body that target unit is aimed at according to the instruction release for receiving for shooting.
Preferably, the target body includes entity target body and/or virtual target body.
Preferably, the virtual target body is that the virtual target body is presented using holographic imaging mode.
Preferably, the target unit of throwing is according to the process of instruction release target body：
Receive control instruction；
The detection position data for throwing target unit；
The entity target body is thrown going out for target unit by the position data and the control instruction according to detection from described
Mouth ejection output.
Preferably, the target unit of throwing is according to the process of instruction release target body：
Receive control instruction；
The detection position data for throwing target unit, the position data includes altitude information, air speed data and number of coordinates
According to；
The position data and the control instruction according to detection use holographic imaging mode output light, to present
State virtual target body.
Preferably, the process of the flying unit carrying throwing target unit flight is：
Receive flight directive；
Position the positional information of the flying unit；
Flown according to the flight directive and the positional information, or
Flown to target location according to the flight directive and the positional information.
The present invention also provides a kind of flight formula and throws target system, and the system includes：
RCU, to output order；
Target unit is thrown, to the target body aimed at for shooting according to the instruction release；
Flying unit, to according to the carrying throwing target unit flight.
The beneficial effect of above-mentioned technical proposal is exemplified below：
Flight formula throwing device is expanded and uses scope, and motion is shot in ad-hoc location without user；
Flight formula throws Target process can control throwing target unit to be taken aim at for shooting according to the instruction release for receiving in flight course
Accurate target body, improves the experience of user；
The instruction control throwing target unit that flight formula is thrown target system and can be sent according to RCU carries out throwing target.
Brief description of the drawings
Fig. 1 is a kind of overall structure diagram of embodiment of flight formula throwing device of the present invention.
Fig. 2 is a kind of module map of embodiment of throwing target unit of the present invention.
Fig. 3 is the module map of another embodiment of throwing target unit of the present invention.
Fig. 4 is method flow diagram of the throwing target unit of the present invention according to a kind of embodiment of instruction release target body.
Fig. 5 is method flow diagram of the throwing target unit of the present invention according to another embodiment of instruction release target body.
Fig. 6 is that flying unit of the present invention carries the method flow diagram for throwing the flight of target unit.
Fig. 7 is a kind of module map of embodiment that flight formula of the present invention throws target system.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.It is based on
Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under the premise of creative work is not made
Embodiment, belongs to the scope of protection of the invention.
It should be noted that in the case where not conflicting, the embodiment in the present invention and the feature in embodiment can phases
Mutually combination.
The invention will be further described with specific embodiment below in conjunction with the accompanying drawings, but not as limiting to the invention.
As shown in figure 1, a kind of flight formula throwing device, the device includes：Flying unit 1 and throwing target unit 2, flying unit
1 carries throwing target unit 2 flies, and throws target unit 2 to according to the instruction release target body for receiving.
In the present embodiment, flight formula throwing device may be implemented in flight course and carry out throwing target using throwing target unit 2, with
Mobile throwing target is realized, the difference according to flying height casts out the target body of different angles, to meet the demand of user, and flight formula
Throwing device is removable to be easy to carry, and expands and uses scope, and motion is shot in ad-hoc location without user.
In a preferred embodiment, flying unit 1 can use rotary wind type flight structure.
In a preferred embodiment, flying unit 1 can use flapping wings type flight structure.
In a preferred embodiment, flying unit 1 can use fixed-wing formula flight structure.
In a preferred embodiment, flying unit 1 can use umbrella wing formula flight structure.
In a preferred embodiment, flying unit 1 can use jet-propelled flight structure.
In a preferred embodiment, flying unit 1 can use dirigible structure.
In a preferred embodiment, target body may include entity target body, and/or virtual target body.
In a preferred embodiment, entity target body uses plate shape structure, loop configuration or rectangular configuration.
In a preferred embodiment, entity target body is the balloon of filling gas.
In a preferred embodiment, entity target body is the target body for being provided with light source.
In a preferred embodiment, virtual target body is the virtual target body presented using optics.
Further, for example and without limitation, virtual target body is that virtual target body is presented using holographic imaging mode.
As shown in Fig. 2 in a preferred embodiment, throwing target unit 2 includes,
First receiver module 21, is used to receive control instruction；
Storage target cabin 22, to storage entities target body；
Ejection portion 23, is used to for entity target body to launch output from the outlet 210 for throwing target unit 2；
First detection module 24, is used to detect the position data for throwing target unit 2；
First control module 25, connects the first receiver module 21, ejection portion 23 and first detection module 24, to root respectively
Launch entity target body in position data and control instruction control the ejection portion 23 detected according to first detection module 24.
Further, for example and without limitation, position data may include altitude information, air speed data and coordinate data.
In the present embodiment, target body is stored using storage target cabin 22, the height for throwing target unit 2 is detected by first detection module 24
Degrees of data, air speed data and coordinate data, the entity target in target cabin 22 will be stored up using the control ejection of the first control module 25 portion 23
Body launches output from the outlet 210 for throwing target unit 2, so as to realize the purpose of the target body that release is aimed at for shooting.
As shown in figure 3, in a preferred embodiment, throwing target unit 2 includes,
Second receiver module 26, is used to receive control instruction；
Emission part 27, is used to using holographic imaging mode output light, so that virtual target body is presented；
Second detection module 28, is used to detect the position data for throwing target unit 2, position data includes altitude information, wind speed
Data and coordinate data；
Second control module 29, connects the second receiver module 26, the detection module 28 of emission part 27 and second, to root respectively
Position data and control instruction the control emission part 27 detected according to the second detection module 28 are imaged.
Further, for example and without limitation, position data may include altitude information, air speed data and coordinate data.
In the present embodiment, altitude information, air speed data and the coordinate for throwing target unit 2 are detected by the second detection module 28
Data, holographic imaging mode output light is used using the control emission part 27 of the second control module 29, so that virtual target body is presented, from
And realize the purpose of the target body that release is aimed at for shooting.
In a preferred embodiment, flying unit 1 includes,
Locating module, to the positional information of positioning flight unit 1；
3rd receiver module, is used to receive flight directive；
Flight module, connects locating module and the 3rd receiver module respectively, to be flown according to flight directive and positional information
OK, or
Flight module is used to be flown to target location according to flight directive and positional information.
In the present embodiment, for example and without limitation, can by the positional information of locating module positioning flight unit 1,
The flight directive that flight module is received according to the 3rd receiver module, performs corresponding flight operation.Throwing target unit 2 can be in flight
Unit 1 discharges target body when being in state of flight；Throw target unit 2 can also discharge target body when flying unit 1 remains static.
In a preferred embodiment, also including image recognition trigger element, image recognition trigger element includes,
First taking module, is used to shoot the image comprising user；
First identification module, to the demand status of identifying user；
First demand determination module, to judge release target body demand according to the image and demand status that shoot.
In the present embodiment, for example and without limitation, can be flown using the technological means of image recognition triggering flying unit 1
OK, thrown when the demand status of the user of the first identification module identification trigger the carrying of flying unit 1 to need to discharge target body demand, then
Target unit 2 takes off from initial position and flies to target location.
In a preferred embodiment, also including voice recognition trigger element, voice recognition trigger element includes,
Second acquisition module, is used to gather the voice signal of user；
Second identification module, to the semantic content of recognition of speech signals；
Second demand determination module, to judge release target body demand according to semantic content.
In the present embodiment, for example and without limitation, can be single using the technological means triggering flight of voice signal identification
Unit 1 flies, and when the semantic content that the second identification module is recognized is release target body demand, then triggers flying unit 1 and carries throwing target list
Unit 2 takes off from initial position and flies to target location.
A kind of flight formula throws Target process, including the step of be：
Flying unit 1 carries throwing target unit 2 and is flown；
Throw the target body that target unit 2 is aimed at according to the instruction release for receiving for shooting.
In the present embodiment, flight formula is thrown Target process and can control to throw target unit 2 according to the finger for receiving in flight course
The target body that order release is aimed at for shooting, improves the experience of user.
In a preferred embodiment, target body may include entity target body and/or virtual target body.
Further, for example and without limitation, virtual target body can be that virtual target body is presented using holographic imaging mode.
As shown in figure 4, in a preferred embodiment, throw target unit is according to the process of instruction release target body：
A1. control instruction is received；
A2. the position data of target unit is thrown in detection；
A3. entity target body is launched output by the position data and control instruction according to detection from the outlet for throwing target unit.
Further, for example and without limitation, position data may include altitude information, air speed data and coordinate data.
In the present embodiment, altitude information, air speed data and the coordinate data of target unit are thrown by detecting, by entity target body
Output is launched from the outlet for throwing target unit, so as to realize the purpose of the target body that release is aimed at for shooting.
As shown in figure 5, in a preferred embodiment, throw target unit is according to the process of instruction release target body：
B1. control instruction is received；
B2. the position data of target unit is thrown in detection, and position data includes altitude information, air speed data and coordinate data；
B3. the position data and control instruction according to detection use holographic imaging mode output light, so that virtual target is presented
Body.
Further, for example and without limitation, position data may include altitude information, air speed data and coordinate data.
In the present embodiment, the altitude information of target unit, air speed data and coordinate data are thrown by detecting, using holography into
Image space formula output light, so that virtual target body is presented, so as to realize the purpose of the target body that release is aimed at for shooting.
As shown in fig. 6, in a preferred embodiment, the process that flying unit carries the unit flight of throwing target is：
C1. flight directive is received；
C2. the positional information of positioning flight unit；
C3. flown according to flight directive and positional information, or
Flown to target location according to flight directive and positional information.
In the present embodiment, for example and without limitation, can be by the positional information of positioning flight unit, flying unit root
According to the flight directive for receiving, corresponding flight operation is performed.Throwing target unit can discharge when flying unit is in state of flight
Target body；Throwing target unit can also discharge target body when flying unit remains static.
In excellent embodiment, throwing before target unit discharges target body according to instruction also includes：
Shoot the image comprising user；
The demand status of identifying user；
Image and demand status according to shooting judge release target body demand.
In the present embodiment, for example and without limitation, can be flown using the technological means of image recognition triggering flying unit
OK, target unit is thrown from initial when the demand status of the user of identification trigger flying unit to need to discharge target body demand, then and carry
Take off and fly to target location in position.
In a preferred embodiment, throwing before target unit discharges target body according to instruction also includes：
Gather the voice signal of user；
The semantic content of recognition of speech signals；
Release target body demand is judged according to semantic content.
In the present embodiment, can be using the technological means triggering flying unit flight of voice signal identification, when the language of identification
Adopted content is release target body demand, then triggering flying unit carrying throwing target unit takes off from initial position and flies to target location.
As shown in fig. 7, a kind of flight formula throws target system, the system includes：
RCU 3, to output order；
Target unit 2 is thrown, to the target body aimed at for shooting according to instruction release；
Flying unit 1, to throw the flight of target unit according to carrying.
In the present embodiment, flight formula is thrown target system and can be thrown according to the instruction control throwing target unit of RCU transmission
Target.
On the basis of above-mentioned technical proposal, further, flying unit can be rotor craft, Fixed Wing AirVehicle or
The aircraft that fixed-wing mixes with rotor.Can be to include one or more spiral if flying unit uses rotor craft
The aircraft of oar, such as helicopter, quadrotor, six rotorcraft, eight-rotary wing aircraft of single propeller etc..Fly
Row unit can automatically fly to target area according to the course data being pre-configured with, it is also possible to receive such as remote control, intelligence
The flight control data that the control devices with radio function such as mobile phone, panel computer, intelligent wearable device send in ground surface end,
And flown to target area based on these flight control datas.
Aircraft generally can also include Power Component, such as horizontal stage electric machine, propeller, propeller motor, and radiating
The mechanical parts such as fan.
Flying unit may also include the winged control plate for controlling flight, and flying control plate includes circuit board and be arranged at circuit board
The upper functional module for being used to realize predetermined function, functional module can include controller module, processor module, sensor assembly
Deng.Further, sensor assembly can include inertia measuring module, temperature sensor module, Height sensor module, distance
Sensor assembly etc..Inertia measuring module includes acceleration transducer and gyroscope, and inertia measuring module can measure nobody
The flight attitude information of aircraft.
In several embodiments provided by the present invention, it should be understood that disclosed relevant apparatus and method, Ke Yitong
Other modes are crossed to realize.For example, device embodiment described above is only schematical, for example, the module or list
The division of unit, only a kind of division of logic function can have other dividing mode when actually realizing, such as multiple units or
Component can be combined or be desirably integrated into another system, or some features can be ignored, or not performed.
The unit that is illustrated as separating component can be or may not be it is physically separate, it is aobvious as unit
The part for showing can be or may not be physical location, you can with positioned at a place, or can also be distributed to multiple
On NE.Some or all of unit therein can be according to the actual needs selected to realize the mesh of this embodiment scheme
's.
In addition, during each functional unit or module in each embodiment of the invention can be integrated in a processing unit,
Can also be that unit is individually physically present, it is also possible to which two or more units are integrated in a unit.Above-mentioned collection
Into unit can both be realized in the form of hardware, it would however also be possible to employ the form of SFU software functional unit is realized.
Embodiments of the invention are the foregoing is only, the scope of the claims of the invention is not thereby limited, it is every to utilize this hair
Equivalent structure or equivalent flow conversion that bright specification and accompanying drawing content are made, or directly or indirectly it is used in other related skills
Art field, is included within the scope of the present invention.
Claims (16)
1. a kind of flight formula throwing device, it is characterised in that the device includes：Flying unit and throwing target unit, the flying unit
The throwing target unit flight is carried, the target unit of throwing is to according to the instruction release target body for receiving.
2. flight formula throwing device according to claim 1, it is characterised in that：The flying unit is flown using rotary wind type
Structure, or
The flying unit uses flapping wings type flight structure, or
The flying unit uses fixed-wing formula flight structure, or
The flying unit uses umbrella wing formula flight structure, or
The flying unit uses jet-propelled flight structure, or
The flying unit uses dirigible structure.
3. flight formula throwing device according to claim 1, it is characterised in that：The target body includes entity target body, and/or
Virtual target body.
4. flight formula throwing device according to claim 3, it is characterised in that：The entity target body uses plate shape knot
Structure, loop configuration or rectangular configuration, or
The entity target body is the balloon of filling gas, or
The entity target body is the target body for being provided with light source.
5. flight formula throwing device according to claim 3, it is characterised in that：The virtual target body is to be presented using optics
Virtual target body.
6. flight formula throwing device according to claim 5, it is characterised in that：The virtual target body is to use holographic imaging
Mode is presented the virtual target body.
7. flight formula throwing device according to claim 3, it is characterised in that：It is described throwing target unit include,
First receiver module, is used to receive control instruction；
Storage target cabin, is used to store the entity target body；
Ejection portion, is used to for the outlet of the entity target body from the throwing target unit to launch output；
First detection module, is used to detect the position data of the throwing target unit；
First control module, connects first receiver module, the ejection portion and the first detection module, to root respectively
The position data detected according to the first detection module and the control instruction control the ejection portion to launch the entity
Target body.
8. flight formula throwing device according to claim 6, it is characterised in that：It is described throwing target unit include,
Second receiver module, is used to receive control instruction；
Emission part, is used to using holographic imaging mode output light, so that the virtual target body is presented；
Second detection module, is used to detect the position data of the throwing target unit, and the position data includes altitude information, wind speed
Data and coordinate data；
Second control module, connects second receiver module, the emission part and second detection module, to root respectively
The position data detected according to second detection module and the control instruction control the emission part to be imaged.
9. flight formula throwing device according to claim 1, it is characterised in that：The flying unit includes,
Locating module, is used to position the positional information of the flying unit；
3rd receiver module, is used to receive flight directive；
Flight module, connects the locating module and the 3rd receiver module, to according to the flight directive and institute respectively
Positional information flight is stated, or
The flight module is used to be flown to target location according to the flight directive and the positional information.
10. a kind of flight formula throws Target process, it is characterised in that including the step of be：
Flying unit carries throwing target unit and is flown；
It is described to throw the target body that target unit is aimed at according to the instruction release for receiving for shooting.
11. flight formulas according to claim 10 throw Target process, it is characterised in that：The target body include entity target body and/
Or virtual target body.
12. flight formulas according to claim 11 throw Target process, it is characterised in that：The virtual target body be using holography into
Image space formula is presented the virtual target body.
13. flight formulas according to claim 11 throw Target process, it is characterised in that：The throwing target unit discharges according to instruction
The process of target body is：
Receive control instruction；
The detection position data for throwing target unit；
According to detection the position data and the control instruction by the entity target body from it is described throwing target unit outlet bullet
Penetrate output.
14. flight formulas according to claim 11 throw Target process, it is characterised in that：The throwing target unit discharges according to instruction
The process of target body is：
Receive control instruction；
The detection position data for throwing target unit, the position data includes altitude information, air speed data and coordinate data；
The position data and the control instruction according to detection use holographic imaging mode output light, so that the void is presented
Intend target body.
15. flight formulas according to claim 10 throw Target process, it is characterised in that：The flying unit is carried throws target unit
The process of flight is：
Receive flight directive；
Position the positional information of the flying unit；
Flown according to the flight directive and the positional information, or
Flown to target location according to the flight directive and the positional information.
A kind of 16. flight formulas throw target system, it is characterised in that the system includes：
RCU, to output order；
Target unit is thrown, to the target body aimed at for shooting according to the instruction release；
Flying unit, to according to the carrying throwing target unit flight.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710002249.XA CN106767180B (en) | 2017-01-03 | 2017-01-03 | Flight formula throwing device throws Target process and system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710002249.XA CN106767180B (en) | 2017-01-03 | 2017-01-03 | Flight formula throwing device throws Target process and system |
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| CN206378060U (en) * | 2017-01-03 | 2017-08-04 | 上海量明科技发展有限公司 | Flight formula throwing device and system |
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2017
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|---|---|---|---|---|
| WO2007015282A1 (en) * | 2005-08-03 | 2007-02-08 | D Adamo Mario | Equipment for target shooting without using live targets |
| US20080192979A1 (en) * | 2006-07-04 | 2008-08-14 | Christopher Bee | Shot pattern and target display |
| KR101034558B1 (en) * | 2009-06-29 | 2011-06-13 | 한국산업기술대학교산학협력단 | Clay Pigeon Shooting Simulation Method, System and Computer-readable Media for Leisure using Screen Image |
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| CN106767180B (en) | 2018-08-24 |
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