CN104635590A - Aircraft, aircraft fight system and fight method - Google Patents
Aircraft, aircraft fight system and fight method Download PDFInfo
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- CN104635590A CN104635590A CN201510057041.9A CN201510057041A CN104635590A CN 104635590 A CN104635590 A CN 104635590A CN 201510057041 A CN201510057041 A CN 201510057041A CN 104635590 A CN104635590 A CN 104635590A
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- 238000000034 method Methods 0.000 title claims abstract description 19
- 238000004891 communication Methods 0.000 claims abstract description 53
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 46
- 229910052744 lithium Inorganic materials 0.000 claims description 46
- 238000001514 detection method Methods 0.000 claims description 20
- 230000005611 electricity Effects 0.000 claims description 12
- 230000002159 abnormal effect Effects 0.000 claims description 10
- 230000007704 transition Effects 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 description 23
- 238000006243 chemical reaction Methods 0.000 description 5
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical group C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
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- 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
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
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- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
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Abstract
The invention discloses an aircraft, an aircraft fight system and a fight method. The aircraft is wirelessly connected with a could server through a wireless communication module, and is communicated with smart terminal equipment through the cloud server; a fly driving module in the aircraft is used for driving the aircraft to fly; a GPS (Global Positioning System) module is used for navigating and acquiring the position information of the aircraft; a camera module is used for acquiring environment image to obtain corresponding image information; an infrared receiving and transmitting module is used for transmitting an infrared laser signal to an enemy aircraft, and is outputting an infrared receiving signal when an infrared laser signal transmitted by the enemy aircraft is received; a main control module is used for transmitting position information, image information, hitting information or hit information corresponding to the infrared receiving signal to the cloud server in order that the smart terminal equipment acquires the position information, the image information, the hitting information and hit information from the cloud server. By adopting the aircraft, the aircraft fight system and the fight method, the aircraft can be applied to fight games in a real scene, and the user experience is enhanced.
Description
Technical field
The present invention relates to telecommunication technique field, particularly relate to a kind of aircraft, aircraft fighting system and battle method.
Background technology
At present, game application miscellaneous emerges in an endless stream, and user can use game application to play game miscellaneous on PC or the intelligent terminal such as mobile phone, IPAD, such as aircraft shooting, racing car etc.But the game played on PC or intelligent terminal is all carry out in virtual scene, such as, when carrying out aircraft shooting, the scene of aircraft and battle is all virtual, and user lacks presence and sense of participation.Along with the development of monitoring technique, aircraft is also applied in reality scene, however the aircraft be applied in reality scene be usually only applied to take photo by plane, forest protection, the monitoring such as the condition of a disaster prospecting application scenario.
Summary of the invention
Fundamental purpose of the present invention is to provide a kind of aircraft, aircraft fighting system and battle method, is intended to realize the battle game of aircraft applications in reality scene, improves user experience.
In order to achieve the above object, the invention provides a kind of aircraft, described aircraft comprises main control module, flight driver module, GPS module, photographing module, wireless communication module and infrared transceiver module; Described flight driver module, GPS module, photographing module, wireless communication module are all connected with described main control module with infrared transceiver module, described aircraft by wireless communication module and cloud server wireless connections, and by cloud server and intelligent terminal communication;
Described flight driver module is for driving aircraft flight;
Described GPS module is used for for aircraft navigation, and obtains the positional information of aircraft;
Described photographing module, for gathering ambient image, obtains the image information that described ambient image is corresponding;
Described infrared transceiver module is used for launching infrared laser signal to enemy aircraft, and when receiving the infrared laser signal that enemy aircraft sends, exports received IR signal to described main control module;
Described main control module is used for described positional information, image information, and the hit information corresponding with described received IR signal or be sent to cloud server by the information of hitting, obtain described positional information, image information for intelligent terminal from cloud server, hit information and hit information.
Preferably, described infrared transceiver module comprises operating voltage input end, control signal input end, received IR signal output terminal, triode, infrared transmitting tube, infrared receiving tube, the first resistance, the second resistance, the 3rd resistance and an electric capacity;
Described operating voltage input end is connected with described electric power management circuit, described control signal input end is all connected with described main control module with described received IR signal output terminal, the base stage of described triode is connected with described control signal input end via described first resistance, and via described capacity earth, the collector of described triode is connected with the negative electrode of described infrared transmitting tube, the grounded emitter of described triode; The anode of described infrared receiving tube is connected with described operating voltage input end via described second resistance; The anode of described infrared transmitting tube is connected with described operating voltage input end, and the negative electrode of described infrared receiving tube is connected with described received IR signal output terminal, and via described 3rd resistance eutral grounding.
Preferably, described aircraft also comprises balance detection module, described balance detection module is used for the equilibrium state of sense aircraft, and export flight abnormal information when detecting that described aircraft is uneven to described main control module, to be exported the state that flight controls signal to described flight driver module adjustment aircraft by main control module.
Preferably, described aircraft also comprises power module, and described power module comprises lithium battery, electric power management circuit and sun power change-over circuit;
Described electric power management circuit is connected with described lithium battery and sun power change-over circuit respectively, and is connected with described main control module, the driver module that flies, GPS module, photographing module, wireless communication module, infrared transceiver module and balance detection module respectively;
Described electric power management circuit is used for the operating voltage of the voltage transitions of lithium battery needed for the modules of aircraft, and monitors the electricity of described lithium battery; Described sun power change-over circuit obtains electric energy when aircraft flight, and is powered by the modules that obtained electric energy exports to lithium cell charging and aircraft by described electric power management circuit.
In addition, in order to achieve the above object, the present invention also provides a kind of aircraft fighting system, and described aircraft fighting system comprises aircraft, cloud server and intelligent terminal, described aircraft and described cloud server wireless connections, described intelligent terminal is connected with cloud server;
Described aircraft comprises main control module, flight driver module, GPS module, photographing module, wireless communication module and infrared transceiver module; Described flight driver module, GPS module, photographing module, wireless communication module are all connected with described main control module with infrared transceiver module, described aircraft by wireless communication module and cloud server wireless connections, and by cloud server and intelligent terminal communication;
Described flight driver module is for driving aircraft flight;
Described GPS module is used for for aircraft navigation, and obtains the positional information of aircraft;
Described photographing module, for gathering ambient image, obtains the image information that described ambient image is corresponding;
Described infrared transceiver module is used for launching infrared laser signal to enemy aircraft, and when receiving the infrared laser signal that enemy aircraft sends, exports received IR signal to described main control module;
Described main control module is used for described positional information, image information, and the hit information corresponding with described received IR signal or be sent to cloud server by the information of hitting;
Described cloud server for receive aircraft send positional information, image information, hit information and hit information;
Described intelligent terminal be used for from cloud server obtain aircraft positional information, image information, hit information and hit information.
Preferably, described infrared transceiver module comprises operating voltage input end, control signal input end, received IR signal output terminal, triode, infrared transmitting tube, infrared receiving tube, the first resistance, the second resistance, the 3rd resistance and an electric capacity;
Described operating voltage input end is connected with described electric power management circuit, described control signal input end is all connected with described main control module with described received IR signal output terminal, the base stage of described triode is connected with described control signal input end via described first resistance, and via described capacity earth, the collector of described triode is connected with the negative electrode of described infrared transmitting tube, the grounded emitter of described triode; The anode of described infrared receiving tube is connected with described operating voltage input end via described second resistance; The anode of described infrared transmitting tube is connected with described operating voltage input end, and the negative electrode of described infrared receiving tube is connected with described received IR signal output terminal, and via described 3rd resistance eutral grounding.
Preferably, described aircraft also comprises balance detection module, described balance detection module is used for the equilibrium state of sense aircraft, and export flight abnormal information when detecting that described aircraft is uneven to described main control module, to be exported the state that flight controls signal to described flight driver module adjustment aircraft by main control module.
Preferably, described aircraft also comprises power module, and described power module comprises lithium battery, electric power management circuit and sun power change-over circuit;
Described electric power management circuit is connected with described lithium battery and sun power change-over circuit respectively, and is connected with described main control module, the driver module that flies, GPS module, photographing module, wireless communication module, infrared transceiver module and balance detection module respectively;
Described electric power management circuit is used for the operating voltage of the voltage transitions of lithium battery needed for the modules of aircraft, and monitors the electricity of described lithium battery; Described sun power change-over circuit obtains electric energy when aircraft flight, and is powered by the modules that obtained electric energy exports to lithium cell charging and aircraft by described electric power management circuit.
In addition, in order to achieve the above object, the present invention also provides a kind of aircraft battle method further, and described aircraft battle method comprises the following steps:
Aircraft is driven during flight at the driver module that flies and is navigated by GPS module, and obtains the positional information of aircraft, gathers ambient image, obtain the image information that described ambient image is corresponding by photographing module;
Described positional information and described image information are sent to cloud server by main control module by aircraft;
Intelligent terminal obtains described positional information and image information from cloud server;
Aircraft launches infrared laser signal by infrared transceiver module to enemy aircraft, and exports received IR signal when receiving the infrared laser signal that enemy aircraft sends;
Aircraft sends the hit information corresponding with described received IR signal by main control module or is sent to cloud server by the information of hitting;
Intelligent terminal hits information and is hit information described in obtaining from cloud server.
Aircraft provided by the invention, aircraft fighting system and battle method, aircraft is by wireless communication module and cloud server wireless connections, and by cloud server and intelligent terminal communication, thus intelligent terminal can obtain the positional information of aircraft between ourselves and the enemy from cloud server, and the image information that one's own side's aircraft obtains, user is by the Aircraft position information between ourselves and the enemy shown by intelligent terminal, and the ambient image corresponding to image information, know the region residing for one's own side's aircraft, and the position of aircraft between ourselves and the enemy, and aircraft increases infrared transceiver module, infrared laser signal is launched to enemy aircraft by infrared transceiver module, and export received IR signal when receiving the infrared laser signal that enemy aircraft sends to main control module, main control module obtains the hit information corresponding with received IR signal according to this received IR signal or is hit information, and information will be hit or be sent to cloud server by the information of hitting, make intelligent terminal can obtain by cloud server the information of hitting and be hit information, thus by the information of hitting shown by intelligent terminal or by the information of hitting, user determines that one's own side's aircraft hits enemy aircraft, or one's own side's aircraft is hit by enemy aircraft, achieve the battle game of aircraft applications in reality scene, improve user experience.
Accompanying drawing explanation
Fig. 1 is the structural representation of aircraft one embodiment of the present invention;
Fig. 2 is the electrical block diagram of infrared transceiver module in aircraft of the present invention;
Fig. 3 is the structural representation of another embodiment of aircraft of the present invention;
Fig. 4 is the structural representation of the another embodiment of aircraft of the present invention;
Fig. 5 is the structural representation of fighting system preferred embodiment of the present invention;
Fig. 6 is the schematic flow sheet that the present invention fights method preferred embodiment.
The realization of object of the present invention, functional characteristics and advantage, will in conjunction with the embodiments, and be described further with reference to accompanying drawing.
Embodiment
Should be appreciated that specific embodiment described herein only in order to explain the present invention, be not intended to limit the present invention.
The invention provides a kind of aircraft.
With reference to the structural representation that Fig. 1, Fig. 1 are aircraft one embodiment of the present invention.
As shown in Figure 1, aircraft of the present invention comprises main control module 100, flight driver module 200, GPS module 300, photographing module 400, wireless communication module 500 and infrared transceiver module 600, flight driver module 200, GPS module 300, photographing module 400, wireless communication module 500 are all connected with main control module 100 with infrared transceiver module 600, main control module 100 is the micro-control unit of aircraft, flight driver module 200 can be motor or motor, and photographing module 400 is video camera camera.Described aircraft passes through wireless communication module 500 and cloud server wireless connections, and by cloud server and intelligent terminal (as mobile phone) communication.
Described flight driver module 200 is for driving aircraft flight.
Described GPS module 300 for being aircraft navigation, and obtains the positional information of aircraft.
Described photographing module 400, for gathering ambient image, obtains the image information that described ambient image is corresponding.
Described infrared transceiver module 600 for launching infrared laser signal to enemy aircraft, and when receiving the infrared laser signal that enemy aircraft sends, exports received IR signal to described main control module 100.
Described main control module 100 is for by described positional information, image information, and the hit information corresponding with described received IR signal or be sent to cloud server by the information of hitting, obtain described positional information, image information for intelligent terminal from cloud server, hit information and hit information.
In the present embodiment, wireless communication module 500 is set on board the aircraft, wireless communication module 500 can be 3G/4G communication module, the wireless communication module of WIFI communication module and other high transfer rate, namely aircraft is by 3G, the wireless networks such as 4G or WIFI and cloud server wireless connections, intelligent terminal is also connected with cloud server, thus aircraft carries out communication by cloud server and intelligent terminal, make the image information of aircraft collection and positional information can be sent to cloud server in real time, intelligent terminal can real-time image acquisition information and positional information show, make user by intelligent terminal Long-distance Control aircraft.
Each aircraft participating in game all has unique mark, and be kept at cloud server, thus user obtains the mark of the aircraft participating in game from cloud server by intelligent terminal, selected one or more aircraft participates in game, i.e. selected enemy aircraft, and set flight time and flight range.
When user uses aircraft to participate in game, user sends flight steering order value cloud server by intelligent terminal, by cloud server, flight steering order is sent to the main control module 100 of aircraft, this flight steering order comprises flight enabled instruction, image capture instruction, navigation instruction, positioning instruction and infrared emission instruction.
Main control module 100 controls signal to flight driver module 200 in the flight steering order received for exporting flight during flight enabled instruction, flight driver module 200 drives aircraft flight according to flight control signal, thus aircraft can be driven according to the direction specified by user, height and speed flight.
Main control module 100 exports shooting and controls signal to photographing module 400 when the flight steering order received is image capture instruction, photographing module 400 is made a video recording to the place that aircraft is gone through according to shooting control signal, namely ambient image is gathered, and obtain image information corresponding to ambient image, obtained image information is sent to main control module 100, by main control module 100, image information is sent to cloud server, thus intelligent terminal can obtain from cloud server the image information that aircraft collects, thus ambient image corresponding to obtained image information can be shown on the display screen of intelligent terminal, thus user can be observed the region that aircraft is gone through.
Main control module 100 exports position control signal and navigational control signals to GPS module 300 when the flight steering order received is navigation instruction, GPS module 300 positions according to the position of position control signal to the current place of aircraft, obtain current positional information, and obtained positional information is sent to main control module 100, by main control module 100, this positional information is sent to cloud server, thus intelligent terminal can obtain from cloud server the positional information that aircraft collects, thus obtained positional information can be shown on the display screen of intelligent terminal, thus user can observe the position at one's own side's aircraft place in the flight range of aircraft.Positional information due to aircraft is sent to cloud server and is kept at cloud server, therefore intelligent terminal can not only obtain the positional information of one's own side's aircraft from cloud server, the positional information of enemy aircraft can also be obtained from cloud server, thus determine the position at one's own side's aircraft and enemy aircraft place, and by the localizing objects position, position at enemy aircraft place.GPS module 300 obtains target location according to navigational control signals, navigates, aircraft is flown to target location, namely fly to enemy aircraft position according to this target location.
User is when observing one's own side's aircraft flight to close enemy aircraft, infrared emission instruction is sent by intelligent terminal, thus main control module 100 exports emissioning controling signal to infrared transmission module when the flight steering order received is infrared emission instruction, infrared transmission module launches infrared laser signal according to this emissioning controling signal to enemy aircraft, namely one's own side's aircraft is shot to enemy aircraft, when infrared transmission module receive enemy aircraft return come infrared laser signal time, infrared transmission module sends received IR signal to main control module 100, according to this received IR signal, main control module 100 is determined that to be now infrared transmission module receive enemy aircraft after launching infrared laser signal and is returned the infrared laser signal come, namely be now that one's own side's aircraft hits enemy aircraft, and send corresponding information of hitting to cloud server, thus intelligent terminal obtains after this hits information from cloud server, show by the mark of the aircraft hit on a display screen, thus according to this mark, user can determine which enemy aircraft is hit.
When main control module 100 does not export emissioning controling signal to infrared transmission module, if main control module 100 receives the received IR signal that infrared transceiver module 600 exports, then main control module 100 determines it is now infrared transmission module receives enemy aircraft and sends infrared laser signal when not launching infrared laser signal according to this received IR signal, namely be now that one's own side's aircraft is hit by enemy aircraft, and send corresponding information of being hit to cloud server, thus intelligent terminal obtains after this is hit information from cloud server, show by the mark of the aircraft hit on a display screen, thus according to this mark, user can determine that one's own side's aircraft is hit.
Aircraft of the present invention is by wireless communication module 500 and cloud server wireless connections, and by cloud server and intelligent terminal communication, thus intelligent terminal can obtain the positional information of aircraft between ourselves and the enemy from cloud server, and the image information that one's own side's aircraft obtains, user is by the Aircraft position information between ourselves and the enemy shown by intelligent terminal, and the ambient image corresponding to image information, know the region residing for one's own side's aircraft, and the position of aircraft between ourselves and the enemy, and aircraft increases infrared transceiver module 600, infrared laser signal is launched to enemy aircraft by infrared transceiver module 600, and export received IR signal when receiving the infrared laser signal that enemy aircraft sends to main control module 100, main control module 100 obtains the hit information corresponding with received IR signal according to this received IR signal or is hit information, and information will be hit or be sent to cloud server by the information of hitting, make intelligent terminal can obtain by cloud server the information of hitting and be hit information, thus by the information of hitting shown by intelligent terminal or by the information of hitting, user determines that one's own side's aircraft hits enemy aircraft, or one's own side's aircraft is hit by enemy aircraft, achieve the battle game of aircraft applications in reality scene, improve user experience.
Refer again to Fig. 2, Fig. 2 is the electrical block diagram of infrared transceiver module 600 in aircraft of the present invention.
Particularly, described infrared transceiver module 600 comprises operating voltage input end VCC, control signal input end VPWM, received IR signal output terminal VDET, triode Q1, infrared transmitting tube D1, infrared receiving tube D2, the first resistance R1, the second resistance R2, the 3rd resistance R3 and electric capacity C1; Wherein, triode Q1 is NPN triode.
Described operating voltage input end VCC is connected with described electric power management circuit 820, described control signal input end VPWM is all connected with described main control module 100 with described received IR signal output terminal VDET, the base stage of described triode Q1 is connected with described control signal input end VPWM via described first resistance R1, and via described electric capacity C1 ground connection, the collector of described triode Q1 is connected with the negative electrode of described infrared transmitting tube D1, the grounded emitter of described triode Q1; The anode of described infrared transmitting tube D1 is connected with described operating voltage input end VCC via described second resistance R2; The anode of described infrared receiving tube D2 is connected with described operating voltage input end VCC, and the negative electrode of described infrared receiving tube D2 is connected with described received IR signal output terminal VDET, and via described 3rd resistance R3 ground connection.
When as shown in Figure 3, main control module 100 exports emissioning controling signal to infrared transmission module when the flight steering order received is infrared emission instruction, this emissioning controling signal is pwm signal, this pwm signal is input to the base stage of triode Q1 through the first resistance R1, thus when pwm signal is high level, triode Q1 conducting, makes infrared transmitting tube D1 conducting, and infrared transmitting tube D1 launches infrared laser signal.When infrared transmitting tube D2 does not receive the infrared laser signal that enemy aircraft sends, infrared transmitting tube D2 ends, received IR signal output terminal VDET is through the 3rd resistance R3 ground connection, the received IR signal that now received IR signal output terminal VDET exports is low level, and namely main control module 100 detects as low level signal; When infrared transmitting tube D2 receives the infrared laser signal that enemy aircraft sends, infrared transmitting tube D2 conducting, the received IR signal that now received IR signal output terminal VDET exports is high level, namely main control module 100 detects as high level signal, and determines that infrared transmitting tube D2 receives infrared laser signal.
Refer again to Fig. 3, Fig. 3 is the structural representation of another embodiment of aircraft of the present invention.
Particularly, described aircraft also comprises balance detection module 700, described balance detection module 700 is for the equilibrium state of sense aircraft, and export flight abnormal information when detecting that described aircraft is uneven to described main control module 100, control signal to export flight by main control module 100 state that described flight driver module 200 adjusts aircraft.
The present embodiment is by the equilibrium state of balance detection module 700 sense aircraft, thus feed back abnormal information to main control module 100 when shake, unstable situation of flying appear in aircraft imbalance and aircraft in flight course, main control module 100 again exports flight according to this abnormal information and controls signal to flight driver module 200, adjusted the state of aircraft by flight driver module 200, aircraft is balanced in flight course.
Refer again to Fig. 4, Fig. 4 is the structural representation of the another embodiment of aircraft of the present invention.
Particularly, described aircraft also comprises power module 800, and described power module 800 comprises lithium battery 810, electric power management circuit 820 and sun power change-over circuit 830.
Described electric power management circuit 820 is connected with described lithium battery 810 and sun power change-over circuit 830 respectively, and respectively with described main control module 100, the driver module 200 that flies, GPS module 300, photographing module 400, wireless communication module 500, infrared transceiver module 600 with balance detection module 700 and be connected.
Described electric power management circuit 820 for by the operating voltage of the voltage transitions of lithium battery 810 needed for the modules of aircraft, and monitors the electricity of described lithium battery 810; Described sun power change-over circuit 830 obtains electric energy when aircraft flight, and to be charged to lithium battery 810 by obtained electric energy by described electric power management circuit 820 and the modules of aircraft is powered.
The voltage that lithium battery 810 provides by electric power management circuit 820 is to required module for power supply, and the voltage provided by lithium battery 810 carries out DC-DC conversion, be converted to multiple voltage to required module for power supply, such as the 3.7V voltage that lithium battery 810 provides is converted to 3.3V, 2.5V, 1.8V etc. respectively, for the modules such as main control module 100, flight driver module 200, GPS module 300, photographing module 400, wireless communication module 500, infrared transceiver module 600 are powered.
Electric power management circuit 820 monitors the electricity of lithium battery 810, with when lithium battery 810 electricity is not enough, is reported to the police by modes such as pilot lamp displays, and then reminding user.
In the present embodiment, sun power change-over circuit 830 is increased at power module 800, obtaining light energy conversion by sun power change-over circuit 830 is that electric energy charges to lithium battery 810, the electricity of supply lithium battery 810 also provides power supply to aircraft, thus the flight time of aircraft can be extended, solve existing aircraft owing to being subject to own wt, impact that lithium battery power supply is supplied with the factors such as limit and the problem that the hang time is not grown.
The present invention also provides a kind of aircraft fighting system.
In conjunction with referring to figs. 1 through Fig. 5, wherein Fig. 5 is the structural representation of aircraft fighting system of the present invention preferred embodiment.
As shown in Figure 5, aircraft fighting system of the present invention comprises aircraft 101, cloud server 102 and intelligent terminal 103 (as mobile phone), described aircraft 101 and the wireless connections of described cloud server 102, described intelligent terminal 103 is connected with cloud server 102.
As shown in Figure 1, described aircraft 101 comprises main control module 100, flight driver module 200, GPS module 300, photographing module 400, wireless communication module 500 and infrared transceiver module 600, described flight driver module 200, GPS module 300, photographing module 400, wireless communication module 500 and infrared transceiver module 600 are all connected with described main control module 100, main control module 100 is the micro-control unit of aircraft 101, flight driver module 200 can be motor or motor, and photographing module 400 is video camera camera.Described aircraft 101 by wireless communication module 500 and cloud server 102 wireless connections, and passes through cloud server 102 and intelligent terminal 103 communication.
Described flight driver module 200 flies for driving aircraft 101.
Described GPS module 300 for navigating for aircraft 101, and obtains the positional information of aircraft 101.
Described photographing module 400, for gathering ambient image, obtains the image information that described ambient image is corresponding.
Described infrared transceiver module 600 for launching infrared laser signal to enemy aircraft, and when receiving the infrared laser signal that enemy aircraft sends, exports received IR signal to described main control module 100.
Described main control module 100 is for by described positional information, image information, and the hit information corresponding with described received IR signal or be sent to cloud server 102 by the information of hitting.
Described cloud server 102 for receive aircraft 101 send positional information, image information, hit information and hit information.
Described intelligent terminal 103 for obtain from cloud server 102 aircraft 101 positional information, image information, hit information and hit information.
In the present embodiment, aircraft 101 arranges wireless communication module 500, wireless communication module 500 can be 3G/4G communication module, the wireless communication module of WIFI communication module and other high transfer rate, namely aircraft 101 is by 3G, the wireless networks such as 4G or WIFI and cloud server 102 wireless connections, intelligent terminal 103 is also connected with cloud server 102, thus aircraft 101 carries out communication by cloud server 102 and intelligent terminal 103, the image information that aircraft 101 is gathered and positional information can be sent to cloud server 102 in real time, intelligent terminal 103 can real-time image acquisition information and positional information show, make user by intelligent terminal 103 Long-distance Control aircraft 101.
Each aircraft 101 participating in game all has unique mark, and be kept at cloud server 102, thus user obtains the mark of the aircraft 101 participating in game from cloud server 102 by intelligent terminal 103, selected one or more aircraft 101 participates in game, i.e. selected enemy aircraft, and set flight time and flight range.
When user uses aircraft 101 to participate in game, user sends flight steering order value cloud server 102 by intelligent terminal 103, by cloud server 102, flight steering order is sent to the main control module 100 of aircraft 101, this flight steering order comprises flight enabled instruction, image capture instruction, navigation instruction, positioning instruction and infrared emission instruction.
Main control module 100 controls signal to flight driver module 200 in the flight steering order received for exporting flight during flight enabled instruction, flight driver module 200 drives aircraft 101 to fly according to flight control signal, thus aircraft 101 can be driven according to the direction specified by user, height and speed flight.
Main control module 100 exports shooting and controls signal to photographing module 400 when the flight steering order received is image capture instruction, photographing module 400 is made a video recording to the place that aircraft 101 is gone through according to shooting control signal, namely ambient image is gathered, and obtain image information corresponding to ambient image, obtained image information is sent to main control module 100, by main control module 100, image information is sent to cloud server 102, thus intelligent terminal 103 can obtain from cloud server 102 image information that aircraft 101 collects, thus ambient image corresponding to obtained image information can be shown on the display screen of intelligent terminal 103, thus user can be observed the region that aircraft 101 is gone through.
Main control module 100 exports position control signal and navigational control signals to GPS module 300 when the flight steering order received is navigation instruction, GPS module 300 positions according to the position of position control signal to the current place of aircraft 101, obtain current positional information, and obtained positional information is sent to main control module 100, by main control module 100, this positional information is sent to cloud server 102, thus intelligent terminal 103 can obtain from cloud server 102 positional information that aircraft 101 collects, thus can obtained positional information be shown on the display screen of intelligent terminal 103, thus user can observe the position at one's own side's aircraft place in the flight range of aircraft 101.Positional information due to aircraft 101 is sent to cloud server 102 and is kept at cloud server 102, therefore intelligent terminal 103 can not only obtain the positional information of one's own side's aircraft from cloud server 102, the positional information of enemy aircraft can also be obtained from cloud server 102, thus determine the position at one's own side's aircraft and enemy aircraft place, and by the localizing objects position, position at enemy aircraft place.GPS module 300 obtains target location according to navigational control signals, navigates according to this target location, makes aircraft 101 to target location flight, namely flies to enemy aircraft position.
User is when observing one's own side's aircraft flight to close enemy aircraft, infrared emission instruction is sent by intelligent terminal, thus main control module 100 exports emissioning controling signal to infrared transmission module when the flight steering order received is infrared emission instruction, infrared transmission module launches infrared laser signal according to this emissioning controling signal to enemy aircraft, namely one's own side's aircraft is shot to enemy aircraft, when infrared transmission module receive enemy aircraft return come infrared laser signal time, infrared transmission module sends received IR signal to main control module 100, according to this received IR signal, main control module 100 is determined that to be now infrared transmission module receive enemy aircraft after launching infrared laser signal and is returned the infrared laser signal come, namely be now that one's own side's aircraft hits enemy aircraft, and send corresponding information of hitting to cloud server 102, thus intelligent terminal 103 obtains after this hits information from cloud server 102, show by the mark of the aircraft 101 hit on a display screen, thus according to this mark, user can determine which enemy aircraft is hit.
When main control module 100 does not export emissioning controling signal to infrared transmission module, if main control module 100 receives the received IR signal that infrared transceiver module 600 exports, then main control module 100 determines it is now infrared transmission module receives enemy aircraft and sends infrared laser signal when not launching infrared laser signal according to this received IR signal, namely be now that one's own side's aircraft is hit by enemy aircraft, and send corresponding information of being hit to cloud server 102, thus intelligent terminal 103 obtains after this is hit information from cloud server 102, show by the mark of the aircraft 101 hit on a display screen, thus according to this mark, user can determine that one's own side's aircraft is hit.
In aircraft fighting system of the present invention, aircraft 101 is by wireless communication module 500 and cloud server 102 wireless connections, and by cloud server 102 and intelligent terminal 103 communication, thus intelligent terminal 103 can obtain the positional information of aircraft 101 between ourselves and the enemy from cloud server 102, and the image information that one's own side's aircraft obtains, user is by aircraft between ourselves and the enemy 101 positional information shown by intelligent terminal 103, and the ambient image corresponding to image information, know the region residing for one's own side's aircraft, and the position of aircraft 101 between ourselves and the enemy, and aircraft 101 increases infrared transceiver module 600, infrared laser signal is launched to enemy aircraft by infrared transceiver module 600, and export received IR signal when receiving the infrared laser signal that enemy aircraft sends to main control module 100, main control module 100 obtains the hit information corresponding with received IR signal according to this received IR signal or is hit information, and information will be hit or be sent to cloud server 102 by the information of hitting, make intelligent terminal 103 can obtain by cloud server 102 information of hitting and be hit information, thus by the information of hitting shown by intelligent terminal 103 or by the information of hitting, user determines that one's own side's aircraft hits enemy aircraft, or one's own side's aircraft is hit by enemy aircraft, achieve aircraft 101 be applied in reality scene battle game, improve user experience.
Particularly, as shown in Figure 2, described infrared transceiver module 600 comprises operating voltage input end VCC, control signal input end VPWM, received IR signal output terminal VDET, triode Q1, infrared transmitting tube D1, infrared receiving tube D2, the first resistance R1, the second resistance R2, the 3rd resistance R3 and electric capacity C1; Wherein, triode Q1 is NPN triode.
Described operating voltage input end VCC is connected with described electric power management circuit 820, described control signal input end VPWM is all connected with described main control module 100 with described received IR signal output terminal VDET, the base stage of described triode Q1 is connected with described control signal input end VPWM via described first resistance R1, and via described electric capacity C1 ground connection, the collector of described triode Q1 is connected with the negative electrode of described infrared transmitting tube D1, the grounded emitter of described triode Q1; The anode of described infrared transmitting tube D1 is connected with described operating voltage input end VCC via described second resistance R2; The anode of described infrared receiving tube D2 is connected with described operating voltage input end VCC, and the negative electrode of described infrared receiving tube D2 is connected with described received IR signal output terminal VDET, and via described 3rd resistance R3 ground connection.
When as shown in Figure 3, main control module 100 exports emissioning controling signal to infrared transmission module when the flight steering order received is infrared emission instruction, this emissioning controling signal is pwm signal, this pwm signal is input to the base stage of triode Q1 through the first resistance R1, thus when pwm signal is high level, triode Q1 conducting, makes infrared transmitting tube D1 conducting, and infrared transmitting tube D1 launches infrared laser signal.When infrared transmitting tube D2 does not receive the infrared laser signal that enemy aircraft sends, infrared transmitting tube D2 ends, received IR signal output terminal VDET is through the 3rd resistance R3 ground connection, the received IR signal that now received IR signal output terminal VDET exports is low level, and namely main control module 100 detects as low level signal; When infrared transmitting tube D2 receives the infrared laser signal that enemy aircraft sends, infrared transmitting tube D2 conducting, the received IR signal that now received IR signal output terminal VDET exports is high level, namely main control module 100 detects as high level signal, and determines that infrared transmitting tube D2 receives infrared laser signal.
Particularly, as shown in Figure 3, described aircraft 101 also comprises balance detection module 700, described balance detection module 700 is for the equilibrium state of sense aircraft 101, exporting flight abnormal information when detecting that described aircraft 101 is uneven to described main control module 100, controlling signal to export flight by main control module 100 state that described flight driver module 200 adjusts aircraft 101.
The present embodiment detects the equilibrium state of unmanned plane 101 by balance detection module 700, thus feed back abnormal information to main control module 100 when shake, unstable situation of flying appear in unmanned plane imbalance and unmanned plane 101 in flight course, main control module 100 again exports flight according to this abnormal information and controls signal to flight driver module 200, adjusted the state of unmanned plane 101 by flight driver module 200, unmanned plane 101 is balanced in flight course.
Particularly, as shown in Figure 4, described aircraft 101 also comprises power module 800, and described power module 800 comprises lithium battery 810, electric power management circuit 820 and sun power change-over circuit 830.
Described electric power management circuit 820 is connected with described lithium battery 810 and sun power change-over circuit 830 respectively, and respectively with described main control module 100, the driver module 200 that flies, GPS module 300, photographing module 400, wireless communication module 500, infrared transceiver module 600 with balance detection module 700 and be connected.
Described electric power management circuit 820 for by the operating voltage of the voltage transitions of lithium battery 810 needed for the modules of aircraft 101, and monitors the electricity of described lithium battery 810; Described sun power change-over circuit 830 obtains electric energy when aircraft 101 flies, and to be charged to lithium battery 810 by obtained electric energy by described electric power management circuit 820 and the modules of aircraft is powered.
The voltage that lithium battery 810 provides by electric power management circuit 820 is to required module for power supply, and the voltage provided by lithium battery 810 carries out DC-DC conversion, be converted to multiple voltage to required module for power supply, such as the 3.7V voltage that lithium battery 810 provides is converted to 3.3V, 2.5V, 1.8V etc. respectively, for the modules such as main control module 100, flight driver module 200, GPS module 300, photographing module 400, wireless communication module 500, infrared transceiver module 600 are powered.
Electric power management circuit 820 monitors the electricity of lithium battery 810, with when lithium battery 810 electricity is not enough, is reported to the police by modes such as pilot lamp displays, and then reminding user.
In the present embodiment, sun power change-over circuit 830 is increased at power module 800, obtaining light energy conversion by sun power change-over circuit 830 is that electric energy charges to lithium battery 810, the electricity of supply lithium battery 810 provides power supply also to aircraft 101, thus the flight time of aircraft 101 can be extended, solve existing aircraft 101 owing to being subject to own wt, impact that lithium battery power supply is supplied with the factors such as limit and the problem that the hang time is not grown.
The present invention also provides a kind of aircraft battle method.
Reference Fig. 6, Fig. 6 are the schematic flow sheet that the present invention fights method preferred embodiment.
Aircraft battle method of the present invention comprises the following steps:
Step S10: aircraft is driven during flight at the driver module that flies and navigated by GPS module, and obtains the positional information of aircraft, gathers ambient image, obtain the image information that described ambient image is corresponding by photographing module.
Step S20: described positional information and described image information are sent to cloud server by main control module by aircraft.
Step S30: intelligent terminal obtains described positional information and image information from cloud server.
When user uses aircraft to participate in game, user sends flight steering order value cloud server by intelligent terminal, by cloud server, flight steering order is sent to the main control module of aircraft, this flight steering order comprises flight enabled instruction, image capture instruction, navigation instruction, positioning instruction and infrared emission instruction.
Main control module controls signal to flight driver module in the flight steering order received for exporting flight during flight enabled instruction, flight driver module drives aircraft flight according to flight control signal, thus aircraft can be driven according to the direction specified by user, height and speed flight.
Main control module exports shooting and controls signal to photographing module when the flight steering order received is image capture instruction, photographing module is made a video recording to the place that aircraft is gone through according to shooting control signal, namely ambient image is gathered, and obtain image information corresponding to ambient image, obtained image information is sent to main control module, by main control module, image information is sent to cloud server, thus intelligent terminal can obtain from cloud server the image information that aircraft collects, thus ambient image corresponding to obtained image information can be shown on the display screen of intelligent terminal, thus user can be observed the region that aircraft is gone through.
Main control module exports position control signal and navigational control signals to GPS module when the flight steering order received is navigation instruction, GPS module positions according to the position of position control signal to the current place of aircraft, obtain current positional information, and obtained positional information is sent to main control module, by main control module, this positional information is sent to cloud server, thus intelligent terminal can obtain from cloud server the positional information that aircraft collects, thus obtained positional information can be shown on the display screen of intelligent terminal, thus user can observe the position at one's own side's aircraft place in the flight range of aircraft.Positional information due to aircraft is sent to cloud server and is kept at cloud server, therefore intelligent terminal can not only obtain the positional information of one's own side's aircraft from cloud server, the positional information of enemy aircraft can also be obtained from cloud server, thus determine the position at one's own side's aircraft and enemy aircraft place, and by the localizing objects position, position at enemy aircraft place.GPS module obtains target location according to navigational control signals, navigates according to this target location, and aircraft is flown to target location, namely flies to enemy aircraft position.
Step S40: aircraft launches infrared laser signal by infrared transceiver module to enemy aircraft, and export received IR signal when receiving the infrared laser signal that enemy aircraft sends.
Step S50: aircraft sends the hit information corresponding with described received IR signal by main control module or is sent to cloud server by the information of hitting.
Step S60: hit information and hit information described in intelligent terminal obtains from cloud server.
User is when observing one's own side's aircraft flight to close enemy aircraft, infrared emission instruction is sent by intelligent terminal, thus main control module exports emissioning controling signal to infrared transmission module when the flight steering order received is infrared emission instruction, infrared transmission module launches infrared laser signal according to this emissioning controling signal to enemy aircraft, namely one's own side's aircraft is shot to enemy aircraft, when infrared transmission module receive enemy aircraft return come infrared laser signal time, infrared transmission module sends received IR signal to main control module, according to this received IR signal, main control module is determined that to be now infrared transmission module receive enemy aircraft after launching infrared laser signal and is returned the infrared laser signal come, namely be now that one's own side's aircraft hits enemy aircraft, and send corresponding information of hitting to cloud server, thus intelligent terminal obtains after this hits information from cloud server, show by the mark of the aircraft hit on a display screen, thus according to this mark, user can determine which enemy aircraft is hit.
When main control module does not export emissioning controling signal to infrared transmission module, if main control module receives the received IR signal that infrared transceiver module exports, then main control module determines it is now infrared transmission module receives enemy aircraft and sends infrared laser signal when not launching infrared laser signal according to this received IR signal, namely be now that one's own side's aircraft is hit by enemy aircraft, and send corresponding information of being hit to cloud server, thus intelligent terminal obtains after this is hit information from cloud server, show by the mark of the aircraft hit on a display screen, thus according to this mark, user can determine that one's own side's aircraft is hit.
Aircraft battle method of the present invention, aircraft is by wireless communication module and cloud server wireless connections, and by cloud server and intelligent terminal communication, thus intelligent terminal can obtain the positional information of aircraft between ourselves and the enemy from cloud server, and the image information that one's own side's aircraft obtains, user is by the Aircraft position information between ourselves and the enemy shown by intelligent terminal, and the ambient image corresponding to image information, know the region residing for one's own side's aircraft, and the position of aircraft between ourselves and the enemy, and aircraft increases infrared transceiver module, infrared laser signal is launched to enemy aircraft by infrared transceiver module, and export received IR signal when receiving the infrared laser signal that enemy aircraft sends to main control module, main control module obtains the hit information corresponding with received IR signal according to this received IR signal or is hit information, and information will be hit or be sent to cloud server by the information of hitting, make intelligent terminal can obtain by cloud server the information of hitting and be hit information, thus by the information of hitting shown by intelligent terminal or by the information of hitting, user determines that one's own side's aircraft hits enemy aircraft, or one's own side's aircraft is hit by enemy aircraft, achieve the battle game of aircraft applications in reality scene, improve user experience.
The foregoing is only the preferred embodiments of the present invention; not thereby the scope of the claims of the present invention is limited; every utilize instructions of the present invention and accompanying drawing content to do equivalent structure or equivalent flow process conversion; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present invention.
Claims (9)
1. an aircraft, it is characterized in that, described aircraft comprises main control module, flight driver module, GPS module, photographing module, wireless communication module and infrared transceiver module, and described flight driver module, GPS module, photographing module, wireless communication module are all connected with described main control module with infrared transceiver module; Described aircraft by wireless communication module and cloud server wireless connections, and by cloud server and intelligent terminal communication;
Described flight driver module is for driving aircraft flight;
Described GPS module is used for for aircraft navigation, and obtains the positional information of aircraft;
Described photographing module, for gathering ambient image, obtains the image information that described ambient image is corresponding;
Described infrared transceiver module is used for launching infrared laser signal to enemy aircraft, and when receiving the infrared laser signal that enemy aircraft sends, exports received IR signal to described main control module;
Described main control module is used for described positional information, image information, and the hit information corresponding with described received IR signal or be sent to cloud server by the information of hitting, obtain described positional information, image information for intelligent terminal from cloud server, hit information and hit information.
2. aircraft as claimed in claim 1, it is characterized in that, described infrared transceiver module comprises operating voltage input end, control signal input end, received IR signal output terminal, triode, infrared transmitting tube, infrared receiving tube, the first resistance, the second resistance, the 3rd resistance and an electric capacity;
Described operating voltage input end is connected with described electric power management circuit, described control signal input end is all connected with described main control module with described received IR signal output terminal, the base stage of described triode is connected with described control signal input end via described first resistance, and via described capacity earth, the collector of described triode is connected with the negative electrode of described infrared transmitting tube, the grounded emitter of described triode; The anode of described infrared receiving tube is connected with described operating voltage input end via described second resistance; The anode of described infrared transmitting tube is connected with described operating voltage input end, and the negative electrode of described infrared receiving tube is connected with described received IR signal output terminal, and via described 3rd resistance eutral grounding.
3. as the aircraft in claim 1 or 2 as described in any one, it is characterized in that, described aircraft also comprises balance detection module, described balance detection module is used for the equilibrium state of sense aircraft, and export flight abnormal information when detecting that described aircraft is uneven to described main control module, to be exported the state that flight controls signal to described flight driver module adjustment aircraft by main control module.
4. aircraft as claimed in claim 3, it is characterized in that, described aircraft also comprises power module, and described power module comprises lithium battery, electric power management circuit and sun power change-over circuit;
Described electric power management circuit is connected with described lithium battery and sun power change-over circuit respectively, and is connected with described main control module, the driver module that flies, GPS module, photographing module, wireless communication module, infrared transceiver module and balance detection module respectively;
Described electric power management circuit is used for the operating voltage of the voltage transitions of lithium battery needed for the modules of aircraft, and monitors the electricity of described lithium battery; Described sun power change-over circuit obtains electric energy when aircraft flight, and is powered by the modules that obtained electric energy exports to lithium cell charging and aircraft by described electric power management circuit.
5. an aircraft fighting system, is characterized in that, described aircraft fighting system comprises aircraft, cloud server and intelligent terminal, described aircraft and described cloud server wireless connections, and described intelligent terminal is connected with cloud server;
Described aircraft comprises main control module, flight driver module, GPS module, photographing module, wireless communication module and infrared transceiver module, and described flight driver module, GPS module, photographing module, wireless communication module are all connected with described main control module with infrared transceiver module; Described aircraft by wireless communication module and cloud server wireless connections, and by cloud server and intelligent terminal communication;
Described flight driver module is for driving aircraft flight;
Described GPS module is used for for aircraft navigation, and obtains the positional information of aircraft;
Described photographing module, for gathering ambient image, obtains the image information that described ambient image is corresponding;
Described infrared transceiver module is used for launching infrared laser signal to enemy aircraft, and when receiving the infrared laser signal that enemy aircraft sends, exports received IR signal to described main control module;
Described main control module is used for described positional information, image information, and the hit information corresponding with described received IR signal or be sent to cloud server by the information of hitting;
Described cloud server for receive aircraft send positional information, image information, hit information and hit information;
Described intelligent terminal be used for from cloud server obtain aircraft positional information, image information, hit information and hit information.
6. aircraft fighting system as claimed in claim 5, it is characterized in that, described infrared transceiver module comprises operating voltage input end, control signal input end, received IR signal output terminal, triode, infrared transmitting tube, infrared receiving tube, the first resistance, the second resistance, the 3rd resistance and an electric capacity;
Described operating voltage input end is connected with described electric power management circuit, described control signal input end is all connected with described main control module with described received IR signal output terminal, the base stage of described triode is connected with described control signal input end via described first resistance, and via described capacity earth, the collector of described triode is connected with the negative electrode of described infrared transmitting tube, the grounded emitter of described triode; The anode of described infrared receiving tube is connected with described operating voltage input end via described second resistance; The anode of described infrared transmitting tube is connected with described operating voltage input end, and the negative electrode of described infrared receiving tube is connected with described received IR signal output terminal, and via described 3rd resistance eutral grounding.
7. the aircraft fighting system as described in claim 5 or 6, it is characterized in that, described aircraft also comprises balance detection module, described balance detection module is used for the equilibrium state of sense aircraft, and export flight abnormal information when detecting that described aircraft is uneven to described main control module, to be exported the state that flight controls signal to described flight driver module adjustment aircraft by main control module.
8. aircraft fighting system as claimed in claim 7, it is characterized in that, described aircraft also comprises power module, and described power module comprises lithium battery, electric power management circuit and sun power change-over circuit;
Described electric power management circuit is connected with described lithium battery and sun power change-over circuit respectively, and is connected with described main control module, the driver module that flies, GPS module, photographing module, wireless communication module, infrared transceiver module and balance detection module respectively;
Described electric power management circuit is used for the operating voltage of the voltage transitions of lithium battery needed for the modules of aircraft, and monitors the electricity of described lithium battery; Described sun power change-over circuit obtains electric energy when aircraft flight, and is powered by the modules that obtained electric energy exports to lithium cell charging and aircraft by described electric power management circuit.
9. an aircraft battle method, is characterized in that, described aircraft battle method comprises the following steps:
Aircraft is driven during flight at the driver module that flies and is navigated by GPS module, and obtains the positional information of aircraft, gathers ambient image, obtain the image information that described ambient image is corresponding by photographing module;
Described positional information and described image information are sent to cloud server by main control module by aircraft;
Intelligent terminal obtains described positional information and image information from cloud server;
Aircraft launches infrared laser signal by infrared transceiver module to enemy aircraft, and exports received IR signal when receiving the infrared laser signal that enemy aircraft sends;
Aircraft sends the hit information corresponding with described received IR signal by main control module or is sent to cloud server by the information of hitting;
Intelligent terminal hits information and is hit information described in obtaining from cloud server.
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