CN205598595U - Volleyball tactics analytic system based on unmanned aerial vehicle - Google Patents

Volleyball tactics analytic system based on unmanned aerial vehicle Download PDF

Info

Publication number
CN205598595U
CN205598595U CN201620410940.2U CN201620410940U CN205598595U CN 205598595 U CN205598595 U CN 205598595U CN 201620410940 U CN201620410940 U CN 201620410940U CN 205598595 U CN205598595 U CN 205598595U
Authority
CN
China
Prior art keywords
gear
teeth
boss
unmanned plane
aerial vehicle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201620410940.2U
Other languages
Chinese (zh)
Inventor
杨秀清
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201620410940.2U priority Critical patent/CN205598595U/en
Application granted granted Critical
Publication of CN205598595U publication Critical patent/CN205598595U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Gear Transmission (AREA)

Abstract

The utility model discloses a volleyball tactics analytic system based on unmanned aerial vehicle, station is handled including unmanned aerial vehicle body, positioning system and ground. Positioning system is fixed in unmanned aerial vehicle body below, handles the station with ground and carries out the data alternating current transmission, and the station is handled with laggard line display of data processing or printing in ground. The utility model discloses simple structure, the cost is lower, and convenient to use is not limited to fixed place. Can effectually keep the stability of unmanned aerial vehicle in the overhead flight in volleyball court. Being convenient for, unmanned aerial vehicle is in time quick to make the action reaction to with data information transmission to ground satellite station. Conveniently train team and vast volleyball fan and carry out real -time data assay and conclusion after competition volleyball tactics.

Description

A kind of vollyball tactical analysis system based on unmanned plane
Technical field
This utility model relates to vollyball tactical analysis system, is specifically related to a kind of vollyball tactics based on unmanned plane and divides Analysis system.
Background technology
Vollyball is the world three one of ball motion significantly, along with continuing to increase of vollyball promotion efficiency, more and more The common people take to this motion.Meanwhile, volleyballer is carried out the data analysis statistical of science, it has also become Improve the important tool of volleyballer's level.Major part vollyball tactical analysis system needs to carry out volleyball court Technological transformation, installs fixing equipment, involves great expense.And the professional standards of overwhelming majority equipment operation require height, It is unfavorable for raising and the popularization of volleyball movement science and technology.Now being badly in need of one can be on any athletic ground, simultaneously Vollyball tactical analysis system simple to operate.
Utility model content
The purpose of this utility model is to overcome above-mentioned deficiency, it is provided that a kind of vollyball tactical analysis based on unmanned plane System, to solve the problems referred to above.
A kind of vollyball tactical analysis system based on unmanned plane, at unmanned plane body, alignment system and ground Reason station.
Described alignment system is fixed on below unmanned plane body, carries out data exchange transmission, ground with floor treatment station Face treating stations carries out showing or printing after data being processed.
Described unmanned plane body includes flight control system, dynamical system, power-supply system, data transmission system, frame And undercarriage.
Described alignment system include the first gear, the second gear, the 3rd gear, the 4th gear, the 5th gear, 6th gear, one or two axles, three or four axles, upper shell, lower house, bearing and DC speed-reducing, mass and Detection module.
Described first gear and the second gear are fixed on one or two axles.First gear and the 6th gear pass for engagement Dynamic.The output shaft of described one or two axles and DC speed-reducing is fixed.
Described second gear and the engagement of the 3rd gear, the second gear and the 3rd gear are engaged transmission.
Described 3rd gear and the 4th gear are fixed on three or four axles.Described first gear and the 4th module phase With, pressure angle is identical.Second number of gear teeth is z2, and the 3rd number of gear teeth is z3, the second number of gear teeth and The ratio of the number of teeth of three number of gear teeth is 3:2.
Described 4th gear and the engagement of the 5th gear, the 4th gear and the 5th gear are engaged transmission.First gear The number of teeth is z1, and the 4th number of gear teeth is z4, and the ratio of the number of teeth of the first number of gear teeth and the 4th number of gear teeth is 2:3.
Described 5th gear top is the gear teeth, and gear teeth central authorities are porose, and bottom is the 5th gear boss, the 5th gear Lobed interior hollow.5th gear boss is connected fixing with mass.
Described 6th gear top is the gear teeth, and bottom is the 6th gear boss.6th gear boss and detection module Connect fixing.Described 6th gear boss in the hollow hole of the 5th gear boss inserted above of the 5th gear, And the 6th gear boss exposes the lower end of the 5th gear.
Described mass is the metal derby with quality, is connected fixing with the 5th gear boss.
Detection module and the 6th gear boss connect fixing.
The position of detection module, from by data receiving system and output transmission system, is read in described floor treatment station Parameter, and receive the real-time pictures of unmanned plane shooting.
The beneficial effects of the utility model are:
This utility model simple in construction, cost is relatively low, easy to use, is not limited to fixed venue.Can be effective Keep unmanned plane in the stability of volleyball court flying overhead.It is easy to unmanned plane and makes movement response quickly, And by data information transfer to earth station.Convenient coach team and vast vollyball fan carry out real-time data analysis With conclusion after competition vollyball tactics.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below will be to reality Execute the required accompanying drawing used in example or description of the prior art to be briefly described, it should be apparent that, describe below In accompanying drawing be only embodiments more of the present utility model, for those of ordinary skill in the art, not On the premise of paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is connection diagram of the present utility model;
Fig. 2 is unmanned plane body schematic diagram of the present utility model;
Fig. 3 is positioning system structure schematic diagram of the present utility model;
Fig. 4 is the 5th gear of the present utility model and the 6th gear schematic diagram.
Marginal data:
1, frame;2, undercarriage;3, alignment system;301, the first gear;302, the second gear;303、 3rd gear;304, the 4th gear;305, the 5th gear;306, the 6th gear;305a, the 5th gear Protruding;306a, the 6th gear boss;311, one or two axle;312, three or four axle;308, upper shell;307、 Bearing;4, mass;5, detection module.
Detailed description of the invention
Below in conjunction with the accompanying drawings preferred embodiment of the present utility model is described in detail, so that of the present utility model Advantage and feature can be easier to be readily appreciated by one skilled in the art, thus make protection domain of the present utility model Apparent clear and definite defining.
See Fig. 1 to Fig. 4, a kind of vollyball tactical analysis system based on unmanned plane, including unmanned plane body, Alignment system 3 and floor treatment station.
Alignment system 3 is fixed on below unmanned plane body, carries out data exchange transmission, ground with floor treatment station Treating stations carries out showing or printing after data being processed.
Unmanned plane body includes flight control system, dynamical system, power-supply system, data transmission system, frame 1 With undercarriage 2.Dynamical system, power-supply system, data transmission system are connected with flight control system.Dynamical system is Unmanned plane body provides power, flight control system to dynamical system control, and then realize direction that flight needs or Set height.Power-supply system is direct current supply lithium battery, can discharge and recharge.Data transmission system includes shooting mould Block and transport module.Taking module shoots downwards, and photographic head minute surface is parallel to the ground, and transport module will be clapped Take the photograph picture transmission to floor treatment station.Undercarriage 2 is fixed on below frame 1.It is fixed with in frame 1 and flies control system System, dynamical system, power-supply system, data transmission system.Undercarriage 2 is fixed on below frame 1.
Alignment system 3 include first gear the 301, second gear the 302, the 3rd gear the 303, the 4th gear 304, 5th gear the 305, the 6th gear 306,1 axle 311,34 axle 312, upper shell 308, lower house, Bearing 307 and DC speed-reducing, mass 4 and detection module 5.First gear the 301, second gear 302, 3rd gear the 303, the 4th gear the 304, the 5th gear the 305, the 6th gear 306,1 axle 311,34 Axle 312 and bearing 307 are positioned at upper shell 308.Lower house structure is symmetrical to upper shell 308 similar, lower casing Body is connected by screw fixing with upper shell 308, by first gear the 301, second gear the 302, the 3rd gear 303, the 4th gear the 304, the 5th gear the 305, the 6th gear 306,1 axle 311,34 axle 312 and Bearing 307 is placed in housing intracavity.DC speed-reducing is fixed on upper shell 308 top.Mass 4 and the 5th Gear boss 305a connects, and detection module 5 is connected with the 6th gear boss 306a.
First gear 301 and the second gear 302 are fixed on one or two axles 311.First gear 301 and the 6th tooth Wheel 306 is engaged transmission.The output shaft of one or two axles 311 and DC speed-reducing is fixed.First gear 301 Modulus is identical, pressure angle is identical with both the 6th gears 306.There are bearing 307, axle in first gear 301 two ends Hold 307 inwalls and one or two axle 311 interference fit.Bearing 307 outer wall and upper shell 308 inner chamber interference fit, First gear 301 can rotate in upper shell 308.There are bearing 307, bearing 307 in second gear 302 two ends Inwall and one or two axle 311 interference fit.Bearing 307 outer wall and upper shell 308 inner chamber interference fit, the first tooth Wheel 301 can rotate in upper shell 308.
Second gear 302 engages with the 3rd gear 303, the second gear 302 with the 3rd gear 303 for engaging biography Dynamic.Modulus is identical, pressure angle is identical with both the 3rd gears 303 for second gear 302.
3rd gear 303 and the 4th gear 304 are fixed on three or four axles 312.First gear 301 and the 4th tooth Taking turns 304 moduluses identical, pressure angle is identical.Second gear 302 number of teeth is z2, and the 3rd gear 303 number of teeth is Z3, second gear 302 number of teeth is 3:2 with the ratio of the number of teeth of the 3rd gear 303 number of teeth.3rd gear 303 liang End has bearing 307, bearing 307 inwall and three or four axle 312 interference fit.Bearing 307 outer wall and upper shell 308 Inner chamber interference fit, the 3rd gear 303 can rotate in upper shell 308.There is bearing at 4th gear 304 two ends 307, bearing 307 inwall and three or four axle 312 interference fit.Bearing 307 outer wall and upper shell 308 inner chamber mistake Being full of cooperation, the 4th gear 304 can rotate in upper shell 308.
4th gear 304 engages with the 5th gear 305, the 4th gear 304 with the 5th gear 305 for engaging biography Dynamic.First gear 301 number of teeth is z1, and the 4th gear 304 number of teeth is z4, first gear 301 number of teeth and the The ratio of the number of teeth of four gear 304 numbers of teeth is 2:3.4th gear 304 is identical with both the 5th gears 305 modulus, Pressure angle is identical.
5th gear 305 top is the gear teeth, and gear teeth central authorities are porose, and bottom is the 5th gear boss 305a, the Five gear boss 305a inner hollow.5th gear boss 305a is connected fixing with mass 4.5th gear There are bearing 307, bearing 307 outer wall and upper shell 308 inner chamber interference fit in the two ends up and down of 305.
6th gear 306 top is the gear teeth, and bottom is the 6th gear boss 306a.6th gear boss 306a It is connected fixing with detection module 5.6th gear boss 306a is from the 5th tooth inserted above of the 5th gear 305 In the hollow hole of the protruding 305a of wheel, and the 6th gear boss 306a exposes the lower end of the 5th gear 305.The There are bearing 307, bearing 307 outer wall and upper shell 308 inner chamber interference fit in the two ends up and down of six gears 306. During installation, bearing 307 is fixed at the 5th gear about 305 two ends, the 6th gear 306 upper and lower side is fixed axle Hold 307.By the 6th gear boss 306a from the 5th gear boss 305a's inserted above of the 5th gear 305 In hollow hole, and the 6th gear boss 306a exposes the lower end of the 5th gear 305.By the 5th gear 305 Insert in upper shell 308 cavity with the 6th gear 306 assembly.By first gear the 301, second gear 302, 3rd gear the 303, the 4th gear 304,1 axle 311 and 34 axle 312 is inserted in upper shell 308 cavity. Upper shell 308 is connected fixing with lower house.
DC speed-reducing rotates forward, and the first gear 301 rotates forward, and is engaged by gear, and the 6th gear 306 inverts, Detection module 5 inverts.First gear 301 rotates forward, and by one or two axle 311 transmissions, the second gear 302 rotates forward, By meshed transmission gear, the 3rd gear 303 inverts, by three or four axle 312 transmissions, the 4th gear 304 Reversion, is engaged by gear, and the 5th gear 305 rotates forward, and mass 4 rotates forward.The rotating forward rotating speed of mass 4 Identical with detection module 5 reverse, mutual balancing moment, keep the stability of unmanned plane body.
Mass 4 is the metal derby with quality, is connected fixing with the 5th gear boss 305a.Mass 4 Can be replaced according to the weight of detection module 5.
Detection module 5 is connected fixing with the 6th gear boss 306a.Detection module 5 constantly detects athlete and wears Wearing the distance of sender unit, and data are wirelessly transmitted to flight control system, flight control system transfers dynamical system, Make unmanned plane the most close to athlete.Transmitter module is zigbee radiating circuit, Bluetooth transmission module.All Accurate indoor positioning can be realized, and athletic position is followed.Require according to accuracy of detection and power is wanted Ask, be replaced different detection modules 5.
The position ginseng of detection module 5, from by data receiving system and output transmission system, is read in floor treatment station Number, and receive the real-time pictures of unmanned plane shooting.After positional information is analyzed by floor treatment station, display is at screen On, and to athletic speed on the scene, position, track carry out data statistics, and simultaneous display is taken a crane shot at unmanned plane In the real-time pictures of shooting.
Athlete puts on transmitter module, and unmanned plane alignment system 3 starts to rotate, and detects transmitter module.Unmanned plane Lift-off of taking off is awaited orders.Volleyball training starts, and detection module 5 constantly detects athlete and wears sender unit Distance, and data are wirelessly transmitted to flight control system, flight control system transfers dynamical system, makes unmanned plane to motion Member is the most close.Detection module 5, from by data receiving system and output transmission system, is read in floor treatment station Location parameter, and receive unmanned plane shooting real-time pictures.Floor treatment station to athletic speed on the scene, Position carries out data statistics, and simultaneous display is taken a crane shot in the real-time pictures shot at unmanned plane, convenient coach team pair Tactical consciousness and the attainment of volleyballer are analyzed.
The above is only preferred implementation of the present utility model, protection domain of the present utility model not only office Being limited to above-described embodiment, all technical schemes belonged under this utility model thinking belong to protection of the present utility model Scope.It should be pointed out that, for those skilled in the art, former without departing from this utility model Some improvements and modifications under reason premise, these improvements and modifications also should be regarded as protection domain of the present utility model.

Claims (3)

1. a vollyball tactical analysis system based on unmanned plane, including unmanned plane body, alignment system (3) With floor treatment station, it is characterised in that: described alignment system (3) is fixed on below unmanned plane body, with ground Face treating stations carries out data transmission, and unmanned plane body includes flight control system, dynamical system, power-supply system, data Transmission system, frame (1) and undercarriage (2), described alignment system (3) include the first gear (301), Second gear (302), the 3rd gear (303), the 4th gear (304), the 5th gear (305), the 6th tooth Wheel (306), one or two axles (311), three or four axles (312), upper shell (308), lower house, bearing (307) With DC speed-reducing, mass (4) and detection module (5), described first gear (301) and the second tooth Wheel (302) be fixed on one or two axles (311), the first gear (301) with the 6th gear (306) for engaging Transmission, the output shaft of described one or two axles (311) and DC speed-reducing fixes, described second gear (302) Engaging with the 3rd gear (303), the second gear (302) and the 3rd gear (303) are engaged transmission, institute State the 3rd gear (303) to be fixed on three or four axles (312) with the 4th gear (304), described first gear (301) identical with the 4th gear (304) modulus, pressure angle is identical, and the second gear (302) number of teeth is z2, 3rd gear (303) number of teeth is z3, the second gear (302) number of teeth and the tooth of the 3rd gear (303) number of teeth The ratio of number is 3:2, and described 4th gear (304) engages with the 5th gear (305), the 4th gear (304) Being engaged transmission with the 5th gear (305), the first gear (301) number of teeth is z1, the 4th gear (304) The number of teeth is z4, and the first gear (301) number of teeth is 2:3 with the ratio of the number of teeth of the 4th gear (304) number of teeth, institute Stating the 5th gear (305) top is the gear teeth, and gear teeth central authorities are porose, and bottom is the 5th gear boss (305a), 5th gear boss (305a) inner hollow, the 5th gear boss (305a) is connected solid with mass (4) Fixed, described 6th gear (306) top is the gear teeth, and bottom is the 6th gear boss (306a), the described 6th Gear boss (306a) is from the hollow of the 5th gear boss (305a) inserted above of the 5th gear (305) In hole, and the 6th gear boss (306a) exposes the lower end of the 5th gear (305).
A kind of vollyball tactical analysis system based on unmanned plane the most according to claim 1, its feature exists In: described mass (4) is the metal derby with quality, is connected fixing with the 5th gear boss (305a).
A kind of vollyball tactical analysis system based on unmanned plane the most according to claim 1, its feature exists In: detection module (5) is connected fixing with the 6th gear boss (306a).
CN201620410940.2U 2016-05-09 2016-05-09 Volleyball tactics analytic system based on unmanned aerial vehicle Expired - Fee Related CN205598595U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620410940.2U CN205598595U (en) 2016-05-09 2016-05-09 Volleyball tactics analytic system based on unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620410940.2U CN205598595U (en) 2016-05-09 2016-05-09 Volleyball tactics analytic system based on unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN205598595U true CN205598595U (en) 2016-09-28

Family

ID=56969441

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620410940.2U Expired - Fee Related CN205598595U (en) 2016-05-09 2016-05-09 Volleyball tactics analytic system based on unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN205598595U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106444888A (en) * 2016-11-17 2017-02-22 广西大学 Humidifying system based on aircraft platform
CN108854031A (en) * 2018-05-29 2018-11-23 深圳臻迪信息技术有限公司 The method and relevant apparatus of exercise data are analyzed by unmanned camera work

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106444888A (en) * 2016-11-17 2017-02-22 广西大学 Humidifying system based on aircraft platform
CN108854031A (en) * 2018-05-29 2018-11-23 深圳臻迪信息技术有限公司 The method and relevant apparatus of exercise data are analyzed by unmanned camera work

Similar Documents

Publication Publication Date Title
CN205598595U (en) Volleyball tactics analytic system based on unmanned aerial vehicle
CN102591350A (en) Flight control method and system of four-rotor unmanned vehicle
CN205785206U (en) A kind of one camera rotary taking device
CN204406207U (en) Based on the system of travelling of unmanned air vehicle technique and head movement capturing technology
CN106004285A (en) Land and air dual-purpose robot
CN204669524U (en) A kind of unmanned plane control system based on mobile Internet
CN106428592A (en) Turnover unmanned aerial vehicle panorama camera
CN209553502U (en) A kind of unmanned plane having gripper
CN206494136U (en) A kind of UAV flight's head
CN104914649A (en) Stabilizer suitable for moving camera shooting
CN201637409U (en) Digital aviation panoramic measuring camera platform
CN207652579U (en) A kind of curling stone hawkeye device
CN107117324A (en) A kind of annular unmanned plane and its aerial device
CN209356927U (en) A kind of polling transmission line UAV system
CN210402057U (en) Portable unmanned aerial vehicle ground satellite station
CN203950104U (en) A kind of adhesion type camera lens is with burnt device
CN106379121A (en) Air-ground synchronous monitoring robot
CN207595281U (en) A kind of unmanned plane full angle image aerial device
CN206602410U (en) A kind of UAS of automatic charging
CN205239910U (en) Remote control flight ware that can fix a point to encircle
CN212637921U (en) Six unmanned aerial vehicle
CN208854618U (en) A kind of wheeled robot for boiler of power plant water-cooling wall Measuring error
CN206281488U (en) A kind of near-earth remote sensing aircraft digital mapping system
CN206431851U (en) A kind of child's gymnastics assisted teaching system
CN110001946A (en) A kind of floated aerial device

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160928

Termination date: 20170509