CN204331334U - A kind of control device - Google Patents
A kind of control device Download PDFInfo
- Publication number
- CN204331334U CN204331334U CN201420831048.2U CN201420831048U CN204331334U CN 204331334 U CN204331334 U CN 204331334U CN 201420831048 U CN201420831048 U CN 201420831048U CN 204331334 U CN204331334 U CN 204331334U
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- China
- Prior art keywords
- catalyzer
- hatch door
- controller
- flight equipment
- positional information
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Abstract
The utility model embodiment discloses a kind of control device, be applied in flight equipment, catalyzer hatch door is the hatch door in described flight equipment storage catalyst cabin, be connected with described controller, described data sink comprises preset control model, described steady arm, for obtaining positional information and the elevation information of described flight equipment, described controller is connected with described steady arm with described data sink respectively, for the positional information that obtains according to described control model and described steady arm and elevation information, described catalyzer hatch door is controlled, visible, by using control model preset in the controller that is connected with catalyzer hatch door and data sink, the positional information of the flight equipment that can obtain according to steady arm and elevation information realize the automatic control to catalyzer hatch door, at suitable height, suitable region releases the catalyzer of fair amount, make when using flight equipment to implement weather modification task, a pilot is only needed to be competent at.
Description
Technical field
The utility model relates to weather modification field, particularly relates to a kind of control device.
Background technology
The shadow is the abbreviation of weather modification, weather modification mainly refers to Appropriate application climate resources, by technological means, artificial affecting is carried out to the physics of local atmosphere, chemical process under proper condition, realize the activity increasing the objects such as sleet, hail suppression, the rain that disappears, fog dispersal, frost prevention.
Under many circumstances, need to use flight equipment when completing weather modification task, catalyzer etc. is broadcasted sowing, to reach the effect of the weather modification of anticipation in the weather modification region of flying predetermined by manipulation flight equipment.When manipulating flight equipment, very high to the personnel requirement on flight equipment, except pilot, also need optional equipment weather modification personnel (being called for short shadow personnel), the cabin door of flight equipment for storage catalyst is controlled, according to the requirement of weather modification task, at proper height by shadow personnel, appropriate area, carries out the opening and closing operations of right times to the hatch door broadcasting sowing the materials such as catalyzer.
Current problem is, two staff (pilot and shadow personnel) all must be equipped with during each enforcement weather modification task, not only be not easy allotment, also can improve the implementation cost of weather modification, cause the efficiency of the practice of weather modification task low thus.
Summary of the invention
In order to solve the problems of the technologies described above, the utility model provides a kind of control device, and making, when using flight equipment to implement weather modification task, only needs pilot one people to complete, saved cost, improve efficiency of the practice.
The utility model embodiment discloses following technical scheme:
A kind of control device, is applied in flight equipment, comprises catalyzer hatch door, data sink, steady arm and controller:
Described catalyzer hatch door is the hatch door in described flight equipment storage catalyst cabin, is connected with described controller, for opening in the control of described controller or closing;
Described data sink comprises preset control model, and described control model comprises the corresponding relation of positional information, elevation information and steering order, and described steering order comprises opening and closing;
Described steady arm, for obtaining positional information and the elevation information of described flight equipment;
Described controller is connected with described steady arm with described data sink respectively, for the positional information that obtains according to described control model and described steady arm and elevation information, controls described catalyzer hatch door.
Preferably, also data transmitter is comprised:
Described data transmitter, for sending control data to described data sink, described control data comprises the corresponding relation of positional information, elevation information and steering order, and described steering order comprises opening and closing;
Described recording controller also for the positional information that obtains according to described control data and described steady arm and elevation information, controls described catalyzer hatch door.
Preferably, described controller comprises time controller, positioner and measurement controller:
Described time controller, for carrying out timing to the state that opens or closes of described catalyzer hatch door;
Described positioner, reaches meet corresponding positional information for controlling described flight equipment, or indicate current positional information requirement;
Described measurement controller, for detecting the quantity of the catalyzer of releasing from described catalyzer hatch door.
Preferably,
Described catalyzer hatch door opens corresponding angle or aperture under the control of described controller.
Preferably,
The described elevation information that described steady arm obtains also comprises the cloud level of described flight equipment region.
Preferably,
Described positional information comprises latitude and longitude information.
Preferably,
The positioning system that described steady arm is equipped by described flight equipment positions.
As can be seen from technique scheme, by using control model preset in the controller that is connected with catalyzer hatch door and data sink, the positional information of the flight equipment that can obtain according to steady arm and elevation information realize the automatic control to catalyzer hatch door, at the catalyzer of suitable height, suitable region releasing fair amount, make when using flight equipment to implement weather modification task, a pilot is only needed to be competent at, be more convenient for allocating, substantially increase the efficiency of the practice of weather modification task.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
The structure drawing of device of a kind of control device that Fig. 1 provides for the utility model embodiment;
The structure drawing of device of a kind of control device that Fig. 2 provides for the utility model embodiment;
The structural representation of a kind of controller that Fig. 3 provides for the utility model embodiment.
Embodiment
In prior art, when needs use flight equipment such as aircraft to perform weather modification task, except pilot, a famous person actor or actress person is also needed to be responsible for controlling the opening and closing of catalyzer hatch door, to discharge the catalyzer of fair amount under suitable condition of work.That is, first the flight equipment of two can only must be used, secondly, each weather modification task especially pop-up mission, all need the order of classes or grades at school of coordination two personnel, allotment gets up difficulty comparatively greatly, even can delay the predetermined spatial domain application time sometimes, cause weather modification task to carry out on time, cause bad impact.For this reason, the utility model provides a kind of control device, by using control model preset in the controller that is connected with catalyzer hatch door and data sink, the positional information of the flight equipment that can obtain according to steady arm and elevation information realize the automatic control to catalyzer hatch door, at the catalyzer of suitable height, suitable region releasing fair amount, make when using flight equipment to implement weather modification task, a pilot is only needed to be competent at, be more convenient for allocating, substantially increase the efficiency of the practice of weather modification task.
For making the object of the utility model embodiment, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the utility model embodiment, technical scheme in the utility model embodiment is clearly described, obviously, described embodiment is the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
The structure drawing of device of a kind of control device that Fig. 1 provides for the utility model embodiment, is applied in flight equipment, comprises catalyzer hatch door 101, data sink 102, steady arm 103 and controller 104:
Described catalyzer hatch door 101 is the hatch door in described flight equipment storage catalyst cabin, is connected with described controller 104, for opening in the control of described controller 104 or closing.
Illustrate, comprise the cabin body of a storage catalyst in flight equipment, general cabin body also has a catalyzer hatch door to be opened/closed towards lower part, and catalyzer hatch door when appropriate machine is opened, release the catalyzer of fair amount, reach the effect of weather modification.Described catalyzer hatch door can be by hinge, opens in rotary manner, and can pass through sliding tray, open in the mode opened to both sides, the utility model does not limit this.For different unfolding mode, optionally, described catalyzer hatch door 101 opens corresponding angle or aperture under the control of described controller 104.
Described data sink 102 comprises preset control model, and described control model comprises the corresponding relation of positional information, elevation information and steering order, and described steering order comprises opening and closing.
Illustrate, described control model can be at region A, opens described catalyzer hatch door 101 time C under the condition of height B, and time C here can by needing the quantity of the catalyzer of release, and the parameters such as the size that described catalyzer hatch door is opened draw.
Described steady arm 103, for obtaining positional information and the elevation information of described flight equipment.
Illustrate, the data obtained by described steady arm 103, the information such as described flight equipment present position and height can be determined, weigh with this described weather modification task of when can implementing, release catalyzer.Wherein, due in a lot of situation, such as rainmaking etc., need catalyzer to drop in carrier, and are generally cloud layers as carrier.Optionally, the described elevation information that described steady arm obtains also comprises the cloud level of described flight equipment region.By detecting cloud layer place height, can understand which highly carry out catalyzer throw in more reasonable.
For described positional information, may be used for the region determining described flight equipment place, optionally, described positional information comprises latitude and longitude information.
In order to more convenient, efficiency is higher, and optionally, the positioning system that described steady arm is equipped by described flight equipment positions.Such as positioned by Airborne GPS.
Described controller 104 is connected with described steady arm 103 with described data sink 102 respectively, for the positional information that obtains according to described control model and described steady arm and elevation information, controls described catalyzer hatch door.
Described controller 104, except using except control model preset in described data sink controls described catalyzer hatch door, can also receive the control data that far-end sends, control described catalyzer hatch door with described control data.Optionally, on the basis of such as embodiment corresponding to Fig. 1, described control device can further include data transmitter 201, as shown in Figure 2, and the structure drawing of device of a kind of control device that Fig. 2 provides for the utility model embodiment.
Described data transmitter 201, for sending control data to described data sink 102, described control data comprises the corresponding relation of positional information, elevation information and steering order, and described steering order comprises opening and closing.
Described recording controller 102 also for the positional information that obtains according to described control data and described steady arm and elevation information, controls described catalyzer hatch door.
Next the inner structure of described controller 104 is conducted further description, as shown in Figure 3, the structural representation of a kind of controller that Fig. 3 provides for the utility model embodiment, described controller 104 comprises time controller 301, positioner 302 and measurement controller 303:
Described time controller 301, for carrying out timing to the state that opens or closes of described catalyzer hatch door.
Described positioner 302, reaches meet corresponding positional information for controlling described flight equipment, or indicate current positional information requirement.
Described measurement controller 303, for detecting the quantity of the catalyzer of releasing from described catalyzer hatch door.
Can be understood as, described time controller 301, positioner 302 and measurement controller 303 are in interconnective relation.
As can be seen from the above-described embodiment, by using control model preset in the controller that is connected with catalyzer hatch door and data sink, the positional information of the flight equipment that can obtain according to steady arm and elevation information realize the automatic control to catalyzer hatch door, at the catalyzer of suitable height, suitable region releasing fair amount, make when using flight equipment to implement weather modification task, a pilot is only needed to be competent at, be more convenient for allocating, substantially increase the efficiency of the practice of weather modification task.
It should be noted that, each embodiment in this instructions all adopts the mode of going forward one by one to describe, between each embodiment identical similar part mutually see, what each embodiment stressed is the difference with other embodiments.Especially, for equipment and system embodiment, because it is substantially similar to embodiment of the method, so describe fairly simple, relevant part illustrates see the part of embodiment of the method.Equipment and system embodiment described above is only schematic, the unit wherein illustrated as separating component or can may not be and physically separates, parts as unit display can be or may not be physical location, namely can be positioned at a place, or also can be distributed in multiple network element.Some or all of module wherein can be selected according to the actual needs to realize the object of the present embodiment scheme.Those of ordinary skill in the art, when not paying creative work, are namely appreciated that and implement.
The above is only preferred implementation of the present utility model, is not intended to limit protection domain of the present utility model.It should be pointed out that for those skilled in the art, under the prerequisite not departing from the utility model principle, can also make some improvements and modifications, these improvements and modifications also should be considered as protection domain of the present utility model.
Claims (7)
1. a control device, is characterized in that, is applied in flight equipment, comprises catalyzer hatch door, data sink, steady arm and controller:
Described catalyzer hatch door is the hatch door in described flight equipment storage catalyst cabin, is connected with described controller, for opening in the control of described controller or closing;
Described data sink comprises preset control model, and described control model comprises the corresponding relation of positional information, elevation information and steering order, and described steering order comprises opening and closing;
Described steady arm, for obtaining positional information and the elevation information of described flight equipment;
Described controller is connected with described steady arm with described data sink respectively, for the positional information that obtains according to described control model and described steady arm and elevation information, controls described catalyzer hatch door.
2. device according to claim 1, is characterized in that, also comprises data transmitter:
Described data transmitter, for sending control data to described data sink, described control data comprises the corresponding relation of positional information, elevation information and steering order, and described steering order comprises opening and closing;
Described recording controller also for the positional information that obtains according to described control data and described steady arm and elevation information, controls described catalyzer hatch door.
3. device according to claim 1 and 2, is characterized in that, described controller comprises time controller, positioner and measurement controller:
Described time controller, for carrying out timing to the state that opens or closes of described catalyzer hatch door;
Described positioner, reaches meet corresponding positional information for controlling described flight equipment, or indicate current positional information requirement;
Described measurement controller, for detecting the quantity of the catalyzer of releasing from described catalyzer hatch door.
4. device according to claim 1, is characterized in that,
Described catalyzer hatch door opens corresponding angle or aperture under the control of described controller.
5. device according to claim 1, is characterized in that,
The described elevation information that described steady arm obtains also comprises the cloud level of described flight equipment region.
6. device according to claim 1, is characterized in that,
Described positional information comprises latitude and longitude information.
7. device according to claim 1, is characterized in that,
The positioning system that described steady arm is equipped by described flight equipment positions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420831048.2U CN204331334U (en) | 2014-12-23 | 2014-12-23 | A kind of control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420831048.2U CN204331334U (en) | 2014-12-23 | 2014-12-23 | A kind of control device |
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| Publication Number | Publication Date |
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| CN204331334U true CN204331334U (en) | 2015-05-13 |
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| CN201420831048.2U Expired - Fee Related CN204331334U (en) | 2014-12-23 | 2014-12-23 | A kind of control device |
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| CN (1) | CN204331334U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019119205A1 (en) * | 2017-12-18 | 2019-06-27 | 深圳市大疆创新科技有限公司 | Hatch door detection method and system, and mobile platform and plant protection machine |
| CN114458119A (en) * | 2021-06-04 | 2022-05-10 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle cabin entry control method, device and system and unmanned aerial vehicle cabin |
| CN114458120A (en) * | 2021-06-04 | 2022-05-10 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle cabin-exiting control method, device and system and unmanned aerial vehicle airport |
-
2014
- 2014-12-23 CN CN201420831048.2U patent/CN204331334U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019119205A1 (en) * | 2017-12-18 | 2019-06-27 | 深圳市大疆创新科技有限公司 | Hatch door detection method and system, and mobile platform and plant protection machine |
| US11408219B2 (en) | 2017-12-18 | 2022-08-09 | SZ DJI Technology Co., Ltd. | Hatch door detection method and system, mobile platform, and plant protection vehicle |
| CN114458119A (en) * | 2021-06-04 | 2022-05-10 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle cabin entry control method, device and system and unmanned aerial vehicle cabin |
| CN114458120A (en) * | 2021-06-04 | 2022-05-10 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle cabin-exiting control method, device and system and unmanned aerial vehicle airport |
| CN114458120B (en) * | 2021-06-04 | 2023-11-17 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle cabin-leaving control method, device and system and unmanned aerial vehicle airport |
| CN114458119B (en) * | 2021-06-04 | 2023-11-17 | 广州极飞科技股份有限公司 | Unmanned aerial vehicle cabin entering control method, device and system and unmanned aerial vehicle cabin |
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Legal Events
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150513 Termination date: 20151223 |
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| EXPY | Termination of patent right or utility model |