CN205809699U - A kind of flight measurement controls device and the unmanned vehicle containing it - Google Patents
A kind of flight measurement controls device and the unmanned vehicle containing it Download PDFInfo
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- CN205809699U CN205809699U CN201620732071.5U CN201620732071U CN205809699U CN 205809699 U CN205809699 U CN 205809699U CN 201620732071 U CN201620732071 U CN 201620732071U CN 205809699 U CN205809699 U CN 205809699U
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Abstract
This utility model relates to unmanned vehicle technical field, it is specifically related to a kind of flight measurement and controls device and the unmanned vehicle containing it, including housing, the inertial measurement cluster being arranged in housing and damping assembly, also include the bottom surface-mounted integrated circuit being arranged in housing, side surface-mounted integrated circuit and static pressure nacelle, described bottom surface-mounted integrated circuit electrically connects with described side surface-mounted integrated circuit, it is formed with cavity in described static pressure nacelle, it is provided with baroport in described static pressure nacelle, described inertial measurement cluster is connected in static pressure nacelle, described bottom surface-mounted integrated circuit electrically connects with described inertial measurement cluster, described damping assembly is connected with static pressure nacelle.This utility model flight measurement controls device compared with conventional use of flight measurement control device, seal is higher, decrease mixed and disorderly air-flow and flight measurement is controlled the impact of device, overall structure is simple, easy for installation, later maintenance is easy, reduces the cost of unmanned vehicle, improves detection and the accuracy controlled.
Description
Technical field
This utility model relates to unmanned vehicle technical field, is specifically related to a kind of flight measurement and controls device and contain it
Unmanned vehicle.
Background technology
Unmanned plane is a kind of unmanned vehicle handled by radio robot or self presetting apparatus.Mesh
Before, along with the development of science and technology, unmanned air vehicle technique reaches its maturity, and unmanned plane is fast with its speed, the feature of flexible operation extensively should
With.In civil area, ground mapping unmanned plane, geological exploration unmanned plane, disaster monitoring unmanned plane, meteorological detection unmanned plane, sky
Middle traffic control unmanned plane, border control unmanned plane, communication relay unmanned plane, pesticide spraying unmanned plane, rescue grinding of unmanned plane
Study carefully and apply the most all in constantly development.
As the control axis of unmanned vehicle, flight measurement controls device and is mainly used in control and the navigation of aircraft,
Normal work to aircraft plays conclusive effect.Calculated by the data that inertia measuring module is recorded and divide
Analysis, flight measurement controls device can control the attitude of aircraft, the position at feedback aircraft place, it is achieved the attitude of aircraft
Control and positioning function.Thereby ensure that the stability of control module is particularly significant.
Along with the development of technology, the application of many rotor unmanned aircrafts is more and more extensive.For many rotor unmanned aircrafts
For, flight measurement controls device and on the one hand requires that weight is little, on the other hand requires to ensure the stability of structure.It is currently used for flying
The control module of row device generally there is problems in that (1) effectiveness in vibration suppression is bad, is vulnerable to the impact of all kinds of shock and vibration, causes
Measurement data is disorderly.(2) structure is complicated, and external interface is many, easy wrong plug interface during use.(3) installation, maintenance difficulty, in a disguised form carries
This flight measurement high controls the cost of device.Therefore, inventing a kind of stability higher, structure design is more reasonable, assembles
Convenient, and the flight measurement being easily installed maintenance controls device, becomes those skilled in the art's technology urgently to be resolved hurrily difficult
Topic.
Utility model content
This utility model is in order to solve above-mentioned technical problem, it is provided that a kind of flight measurement for unmanned vehicle controls dress
Putting, effectively reduce the output noise of Mierotubule-associated proteins, and eliminate the impact on baroceptor of the mixed and disorderly air-flow, permanent use should
Device, still is able to be in optimum Working.
In order to reach above-mentioned technique effect, this utility model includes techniques below scheme:
A kind of flight measurement controls device, the inertial measurement cluster including housing, being arranged in housing and damping assembly, goes back
Including the bottom surface-mounted integrated circuit being arranged in housing, side surface-mounted integrated circuit and static pressure nacelle, described bottom surface-mounted integrated circuit
Electrically connecting with described side surface-mounted integrated circuit, be formed with cavity in described static pressure nacelle, described inertial measurement cluster is connected to quiet
In ballasting body, described bottom surface-mounted integrated circuit electrically connects with described inertial measurement cluster, and described damping assembly is with static pressure nacelle even
Connect.
It is reasonable in design that this utility model flight measurement controls apparatus structure, the design of said structure, effectively reduces vibration right
Flight measurement controls the impact that device produces, and can also completely cut off high velocity air simultaneously, and inertial measurement cluster is equipped with dampening assembly, these
Design all decreases vibrates the impact that flight measurement controls device, improves stability further, thus improves the essence of measurement
Degree.
The level of bottom surface-mounted integrated circuit can avoid DATA REASONING error, improves certainty of measurement；Side surface-mounted integrated circuit
Combination with bottom surface-mounted integrated circuit is connected, and on the one hand facilitates the plug of interface, on the other hand it also avoid the integrated electricity in bottom
The deformation of road plate, improves the service life of block mold.
Further, described static pressure nacelle is provided with baroport；Described bottom surface-mounted integrated circuit passes through pricking with needle with described
Side surface-mounted integrated circuit connects；Connecting on described side surface-mounted integrated circuit and have multiple output port, described output port is with outer
The equipment that connects connects.
Further, described housing includes interconnective upper shell and lower house；Described upper shell and lower house and side
The edge that limit surface-mounted integrated circuit contacts is relatively set with stopper slot I and stopper slot II respectively, when upper shell connects with lower house
When connecing, described output port is positioned at described stopper slot I and stopper slot II.
The design of stopper slot I and stopper slot II is prevented effectively from output port wiring wrong plug, and then ensures the safety used.
Further, described upper shell and lower house clamping；
It is formed with reinforcement in described upper cover body, described reinforcement is formed stopper slot III, arrange in described lower cover
Limited location groove IV, when described upper shell is connected with lower house, described side surface-mounted integrated circuit is connected in stopper slot III and spacing
In groove IV；
Described housing is cube, and four angles of described upper shell and lower house are provided with boss, on described boss
Being provided with fixing hole, the fixing hole of described upper shell is connected with the fixing hole of lower house by fixture.
By boss, fixing hole and the design of fixture, upper-lower casing is made to define stable and the most airtight cavity, from
And completely cut off the impact that inertia measuring module is produced by the most mixed and disorderly air-flow.
The design of strong muscle adds integrally-built intensity, also defines the cavity of an opposing seal in enclosure interior.
In addition, reinforcement also acts as the effect of fixing side surface-mounted integrated circuit.During assembling, can be by side surface-mounted integrated circuit along adding
Strong muscle is slidably installed into upper shell, and the inclined-plane bottom reinforcement makes alignment become convenient.
Stopper slot III and the design of stopper slot IV simultaneously, it is ensured that the level of bottom surface-mounted integrated circuit and side integrated circuit
Plate vertical, limits bottom surface-mounted integrated circuit and the displacement of side surface-mounted integrated circuit simultaneously.Surface-mounted integrated circuit bottom guarantee
Level can avoid DATA REASONING error, improves certainty of measurement；Ensure that on the one hand the vertical of side surface-mounted integrated circuit then facilitate
The plug of interface, on the other hand it also avoid the deformation of bottom surface-mounted integrated circuit, improves the service life of block mold.
Further, a bottom surface-mounted integrated circuit and two side surface-mounted integrated circuits is installed in described housing, two
Side surface-mounted integrated circuit is respectively perpendicular and is connected on two sides that bottom surface-mounted integrated circuit is relative.
Further, described inertial measurement cluster includes interconnective surface-mounted integrated circuit and inertial sensor, described
Surface-mounted integrated circuit baroport it is provided with on surface-mounted integrated circuit.
Further, described surface-mounted integrated circuit is electrically connected with bottom surface-mounted integrated circuit by soft arranging wire.
Further, described damping assembly includes the first cushion and the second cushion, described first cushion, static pressure
Nacelle and the second cushion are sequentially connected with；Described bottom surface-mounted integrated circuit is connected with described second cushion.
A kind of unmanned vehicle, controls device including above-mentioned flight measurement.
Use technique scheme, including following beneficial effect: this utility model provides a kind of flight measurement to control device
And the unmanned vehicle containing it, wherein flight measurement control apparatus structure is reasonable in design, fully limits the position of surface-mounted integrated circuit
Move, enable stable being arranged in housing of surface-mounted integrated circuit.It is integrated that this utility model flight measurement controls device whole height
Change, it is simple to integrated with other device systems.Compared with controlling device with conventional use of flight measurement, device of the present utility model
Seal is strong, decreases mixed and disorderly air-flow and flight measurement controls the impact of device, and overall structure is simple, easy for installation, and the later stage ties up
Protect easily, reduce the cost of unmanned vehicle, improve detection and the accuracy controlled.
Accompanying drawing explanation
Fig. 1 is that this utility model embodiment flight measurement controls device explosion structure chart；
Fig. 2 is the internal structure front view that flight measurement shown in this utility model Fig. 1 controls device；
Fig. 3 is that this utility model connects the bottom surface-mounted integrated circuit top view having static pressure nacelle；
Fig. 4 is this utility model lower cover structural representation；
Fig. 5 is this utility model upper cover body structural representation.
In figure,
1, upper shell；11, boss I；12, fixing hole I；13, stopper slot I；14, horizontal ledge I；15, reinforcement；16, oblique
Face；17, stopper slot III；18, edge lug boss I；2, side surface-mounted integrated circuit；21, output port；22, pricking with needle；3, bottom is integrated
Circuit board；4, the first cushion blocking；5, static pressure nacelle；51, baroport；52, soft arranging wire；6, the second cushion blocking；7, lower house；71、
Edge lug boss II；72, boss II；73, fixing hole II；74, stopper slot II；75, stopper slot IV；76, horizontal ledge II；8, spiral shell
Silk.
Detailed description of the invention
Below by specific embodiment and combine accompanying drawing this utility model is described in further detail.
Embodiment:
The present embodiment provides a kind of flight measurement to control device, as it is shown in figure 1, include housing, be arranged in housing used
Property measure assembly and damping assembly, the bottom surface-mounted integrated circuit 3 that also includes being arranged in housing, side surface-mounted integrated circuit 2 and quiet
Ballasting body 5, described bottom surface-mounted integrated circuit electrically connects with described side surface-mounted integrated circuit, is formed free in described static pressure nacelle
Chamber, described inertial measurement cluster is connected in static pressure nacelle, and described bottom surface-mounted integrated circuit is electrically connected with described inertial measurement cluster
Connecing, described damping assembly is connected with static pressure nacelle
In the present embodiment, further, as shown in Figures 2 and 3, described static pressure nacelle is provided with baroport 51；Institute
State bottom surface-mounted integrated circuit to be connected with described side surface-mounted integrated circuit by pricking with needle 22；Connect on described side surface-mounted integrated circuit
Having multiple output port 21, described output port is connected with external equipment.
In the present embodiment, further, as it is shown in figure 1, described housing includes interconnective upper shell 1 and lower house
7；The edge that described upper shell and lower house contact with side surface-mounted integrated circuit is relatively set with stopper slot I13 and limit respectively
Position groove II74, when upper shell is connected with lower house, described output port is positioned at described stopper slot I and stopper slot II.Such as Fig. 4
Shown in Fig. 5, described upper shell is provided with stopper slot I13, described lower house is provided with stopper slot II74.
In the present embodiment, further, as it is shown in figure 1, described upper shell and lower house clamping；
As shown in Figure 4 and Figure 5, it is formed with reinforcement 15 in described upper cover body, described reinforcement is formed with stopper slot
III17, is provided with stopper slot IV75 in described lower cover, when described upper shell is connected with lower house, and the integrated electricity of described side
Road board is connected in stopper slot III and stopper slot IV.Described upper shell interior side edge is provided with edge lug boss I18, described
Lower house interior side edge is provided with the edge lug boss II71 matched with edge lug boss I, when needs are by upper shell and lower casing
When body connects, by edge lug boss I and edge lug boss II clamping；The edge part of described reinforcement is formed with inclined-plane 16.Described upper casing
It is internally formed horizontal ledge I14, so lower casing has been internally formed horizontal ledge II76, when described upper shell is connected with lower house
Time, described bottom surface-mounted integrated circuit and two horizontal ledge contact, and bottom surface-mounted integrated circuit is played spacing effect.
In the present embodiment, further, as shown in Figure 4 and Figure 5, described housing is cube, described upper shell and
Four angles of lower house are provided with boss, and described boss is provided with fixing hole, and the fixing hole of described upper shell is by fixing
Part is connected with the fixing hole of lower house.
Concrete, four angles of described upper shell are provided with boss I11, boss I11 is provided with fixing hole I12, institute
State and be provided with boss II72 on four angles of lower house, boss II72 is provided with fixing hole II73, described fixing hole I and fixes
Hole II is screw hole, and described fixture is screw 8, is connected fixing to upper shell and lower house by screw, makes housing be formed
Stable and the most airtight cavity.
In the present embodiment, further, as it is shown in figure 1, be provided with in described housing one bottom surface-mounted integrated circuit and
Two side surface-mounted integrated circuits, two side surface-mounted integrated circuits are respectively perpendicular and are connected to two sides that bottom surface-mounted integrated circuit is relative
Bian Shang.When upper shell is connected with lower house, described bottom surface-mounted integrated circuit contacts with horizontal ledge, to bottom integrated circuit
Plate produces spacing effect, and side surface-mounted integrated circuit the most of the present utility model is positioned at stopper slot III and stopper slot IV, makes the end
Portion's integrated circuit is originally firm with side surface-mounted integrated circuit to be connected, and is formed and stablizes plumbness.
In the present embodiment, further, described inertial measurement cluster includes interconnective surface-mounted integrated circuit and is used to
Property sensor, described surface-mounted integrated circuit is provided with surface-mounted integrated circuit baroport.
In the present embodiment, further, as it is shown on figure 3, described surface-mounted integrated circuit is integrated with bottom by soft arranging wire 52
Circuit board electrically connects.
In the present embodiment, further, as it is shown in figure 1, described damping assembly includes that the first cushion 4 and second subtracts
Shake pad 6, described first cushion, static pressure nacelle and the second cushion are sequentially connected with；Described bottom surface-mounted integrated circuit and described the
Two cushions connect.
The present embodiment provides a kind of unmanned vehicle, controls device including above-mentioned flight measurement.
The foregoing is only preferred embodiment of the present utility model, be not limited to this utility model, for this
For the technical staff in field, this utility model can have various modifications and variations.All in spirit of the present utility model and principle
Within, any modification, equivalent substitution and improvement etc. made, within should be included in protection domain of the present utility model.
Claims (10)
1. flight measurement controls a device, the inertial measurement cluster including housing, being arranged in housing and damping assembly, and it is special
Levy and be, also include bottom surface-mounted integrated circuit (3), side surface-mounted integrated circuit (2) and the static pressure nacelle (5) being arranged in housing,
Described bottom surface-mounted integrated circuit electrically connects with described side surface-mounted integrated circuit, is formed with cavity in described static pressure nacelle, described used
Property measure assembly be connected in static pressure nacelle, described bottom surface-mounted integrated circuit electrically connects with described inertial measurement cluster, described in subtract
The assembly that shakes is connected with static pressure nacelle.
Flight measurement the most according to claim 1 controls device, it is characterised in that be provided with static pressure in described static pressure nacelle
Hole (51)；Described bottom surface-mounted integrated circuit is connected with described side surface-mounted integrated circuit by pricking with needle (22)；Described side is integrated
Connecting on circuit board and have multiple output port (21), described output port is connected with external equipment.
Flight measurement the most according to claim 2 controls device, it is characterised in that described housing includes on interconnective
Housing (1) and lower house (7)；Described upper shell is the most relative with the edge that side surface-mounted integrated circuit contacts with lower house to be set
Being equipped with stopper slot I (13) and stopper slot II (74), when upper shell is connected with lower house, described output port is positioned at described spacing
In groove I and stopper slot II.
Flight measurement the most according to claim 3 controls device, it is characterised in that described upper shell and lower house card
Connect；
It is formed with reinforcement (15) in described upper shell, described reinforcement is formed with stopper slot III (17), in described lower house
Being provided with stopper slot IV (75), when described upper shell is connected with lower house, described side surface-mounted integrated circuit is connected in stopper slot
In III and stopper slot IV.
Flight measurement the most according to claim 3 controls device, it is characterised in that described housing is cube, described
Four angles of upper shell and lower house are provided with boss, and described boss is provided with fixing hole, the fixing hole of described upper shell
It is connected with the fixing hole of lower house by fixture.
6. control device according to the flight measurement described in any one of Claims 1 to 5, it is characterised in that install in described housing
A bottom surface-mounted integrated circuit and two side surface-mounted integrated circuits, two side surface-mounted integrated circuits are had to be respectively perpendicular and be connected to bottom
On two sides that surface-mounted integrated circuit is relative.
Flight measurement the most according to claim 1 controls device, it is characterised in that described inertial measurement cluster includes phase
The surface-mounted integrated circuit connected and inertial sensor, described surface-mounted integrated circuit is provided with surface-mounted integrated circuit baroport.
Flight measurement the most according to claim 7 controls device, it is characterised in that described surface-mounted integrated circuit passes through soft arranging wire
(52) electrically connect with bottom surface-mounted integrated circuit.
Flight measurement the most according to claim 1 controls device, it is characterised in that described damping assembly includes that first subtracts
Shake pad (4) and the second cushion (6), described first cushion, static pressure nacelle and the second cushion are sequentially connected with；Described bottom collection
Circuit board is become to be connected with described second cushion.
10. a unmanned vehicle, it is characterised in that include that the flight measurement described in any one of claim 1～9 controls dress
Put.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620732071.5U CN205809699U (en) | 2016-07-12 | 2016-07-12 | A kind of flight measurement controls device and the unmanned vehicle containing it |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620732071.5U CN205809699U (en) | 2016-07-12 | 2016-07-12 | A kind of flight measurement controls device and the unmanned vehicle containing it |
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| Publication Number | Publication Date |
|---|---|
| CN205809699U true CN205809699U (en) | 2016-12-14 |
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|---|---|---|---|
| CN201620732071.5U Active CN205809699U (en) | 2016-07-12 | 2016-07-12 | A kind of flight measurement controls device and the unmanned vehicle containing it |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106896823A (en) * | 2017-04-28 | 2017-06-27 | 上海拓攻机器人有限公司 | The control device and unmanned vehicle of unmanned vehicle |
| CN107172840A (en) * | 2017-06-08 | 2017-09-15 | 歌尔科技有限公司 | A kind of heat-insulated fixed structure of head Camera Inertial Measurement Units |
| CN108839808A (en) * | 2018-07-05 | 2018-11-20 | 上海歌尔泰克机器人有限公司 | Flight control assemblies and unmanned vehicle |
| WO2019127356A1 (en) * | 2017-12-29 | 2019-07-04 | 深圳市大疆创新科技有限公司 | Centre plate unit and unmanned aerial vehicle |
| CN113252294A (en) * | 2021-06-16 | 2021-08-13 | 西南交通大学 | Cross-sea bridge space wind speed and direction testing system and monitoring method |
-
2016
- 2016-07-12 CN CN201620732071.5U patent/CN205809699U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106896823A (en) * | 2017-04-28 | 2017-06-27 | 上海拓攻机器人有限公司 | The control device and unmanned vehicle of unmanned vehicle |
| CN106896823B (en) * | 2017-04-28 | 2018-09-21 | 上海拓攻机器人有限公司 | The control device and unmanned vehicle of unmanned vehicle |
| WO2018196043A1 (en) * | 2017-04-28 | 2018-11-01 | 上海拓攻机器人有限公司 | Control apparatus for unmanned aerial vehicle, and unmanned aerial vehicle |
| EP3432111A4 (en) * | 2017-04-28 | 2020-01-01 | Shanghai Topxgun Robotics Co., Ltd. | Control apparatus for unmanned aerial vehicle, and unmanned aerial vehicle |
| US11032906B2 (en) | 2017-04-28 | 2021-06-08 | Shanghai TopxGun Robotics Co., Ltd. | Control device for unmanned aerial vehicle and unmanned aerial vehicle |
| CN107172840A (en) * | 2017-06-08 | 2017-09-15 | 歌尔科技有限公司 | A kind of heat-insulated fixed structure of head Camera Inertial Measurement Units |
| WO2019127356A1 (en) * | 2017-12-29 | 2019-07-04 | 深圳市大疆创新科技有限公司 | Centre plate unit and unmanned aerial vehicle |
| CN108839808A (en) * | 2018-07-05 | 2018-11-20 | 上海歌尔泰克机器人有限公司 | Flight control assemblies and unmanned vehicle |
| CN113252294A (en) * | 2021-06-16 | 2021-08-13 | 西南交通大学 | Cross-sea bridge space wind speed and direction testing system and monitoring method |
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