CN212229451U - Control terminal for controlling wireless remote control aircraft - Google Patents
Control terminal for controlling wireless remote control aircraft Download PDFInfo
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- CN212229451U CN212229451U CN202020880029.4U CN202020880029U CN212229451U CN 212229451 U CN212229451 U CN 212229451U CN 202020880029 U CN202020880029 U CN 202020880029U CN 212229451 U CN212229451 U CN 212229451U
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Abstract
The application discloses a control terminal for controlling a wireless remote control aircraft. The control terminal includes: the system comprises a main control module, a sensor module, a positioning module, an acquisition module, a wireless communication module, a fan control module and an intelligent end; the sensor module is connected with the main control module, the main control module is connected with the positioning module, the acquisition module, the wireless communication module and the fan control module, and the wireless communication module is connected with the intelligent terminal; the sensor module includes: the device comprises an angular velocity sensor, an acceleration sensor and a distance sensor, wherein the angular velocity sensor, the acceleration sensor and the distance sensor are arranged on an aircraft. This application has been solved and has been adopted a plurality of rockers to input flight control instruction to because user and unmanned vehicles are the separation in physics, the control degree of difficulty is high and complex operation's problem.
Description
Technical Field
The utility model relates to an aircraft technical field particularly, relates to a control terminal for controlling wireless remote control aircraft.
Background
As unmanned aerial vehicles have moved into the consumer market, particularly multi-rotor aircraft, typically quad multi-rotor aircraft, have become the preferred means of performing aerial photography. With the further subdivision of the application market and the field of aerial photography of unmanned aerial vehicles, daily consumption-level unmanned aerial vehicles are being separated from professional consumption-level unmanned aerial vehicles, and self-photographing unmanned aerial vehicles which are miniaturized, portable and simple to operate appear. Unmanned vehicles, especially aerial vehicles, have begun to be widely noticed and popularized, but actual use by consumers still reflects that the aerial vehicles are too difficult to control, and market prospects of the aerial vehicles are affected.
However, the current control method of the unmanned aerial vehicle still generally adopts a rocker control mode, a user needs to input flight control instructions by adopting a plurality of rockers in a direction with at least 6 degrees of freedom in space, and because the user is physically separated from the unmanned aerial vehicle, the user also needs to have the capability of taking the spatial position of the unmanned aerial vehicle into consideration when controlling the unmanned aerial vehicle, and only then can well control the unmanned aerial vehicle.
Aiming at the problems that a plurality of rockers are adopted to input flight control instructions in the prior art, and a user is physically separated from an unmanned aerial vehicle, so that the control difficulty is high and the operation is complex, an effective solution is not provided at present.
SUMMERY OF THE UTILITY MODEL
The main aim at of this application provides a control terminal for controlling wireless remote control aircraft to solve and adopt a plurality of rockers to input flight control instruction, and because user and unmanned vehicles are the separation in physics, the control degree of difficulty is high and complex operation's problem.
In order to achieve the above object, according to one aspect of the present application, there is provided a control terminal for controlling a wireless remote-controlled aerial vehicle.
A control terminal for controlling a wireless remote-controlled aerial vehicle according to the application, comprising: the system comprises a main control module, a sensor module, a positioning module, an acquisition module, a wireless communication module, a fan control module and an intelligent end; the sensor module is connected with the main control module, the main control module is connected with the positioning module, the acquisition module, the wireless communication module and the fan control module, and the wireless communication module is connected with the intelligent terminal; the sensor module includes: the device comprises an angular velocity sensor, an acceleration sensor and a distance sensor, wherein the angular velocity sensor, the acceleration sensor and the distance sensor are arranged on an aircraft; the acquisition module comprises: the vision module is arranged on the aircraft, and the voice module is arranged on the control terminal; the main control module is used for sending control signals to control the sensor module, the positioning module, the acquisition module, the wireless communication module and the fan control module to act; the wireless communication module is used for transmitting a wireless signal to the intelligent terminal; the intelligent terminal comprises: the intelligent mobile phone APP comprises a smart mobile phone APP, a computer client and an LED display screen, and is used for receiving signals.
Further, the method also comprises the following steps: and the power supply module is electrically connected with the main control module.
Further, the power module is a solar panel.
Further, the vision module is a high-definition camera.
Furthermore, the model of the high-definition camera is TC-NC9010S 2-MP.
Further, the wireless communication module is one or more of WIFI, ZigBee, Bluetooth and RFID.
Further, the model of the main control module is STC90C52 AD.
Furthermore, the positioning module is used for GPS positioning or Beidou positioning.
In this application embodiment, adopt host system wireless control's mode, through being connected sensor module and host system, host system and orientation module, collection module, wireless communication module and fan control module are connected, wireless communication module is connected with the intelligent end, wireless control's purpose has been reached, thereby realized the control degree of difficulty low with the simple operation's technological effect, and then solved and adopted a plurality of rockers to input flight control instruction, and because user and unmanned vehicles are separated in physics, control degree of difficulty height and complex operation's technical problem.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, serve to provide a further understanding of the application and to enable other features, objects, and advantages of the application to be more apparent. The drawings and their description illustrate the embodiments of the invention and do not limit it. In the drawings:
fig. 1 is a schematic view of a control terminal for controlling a wireless remote control aircraft according to the present invention;
fig. 2 is a schematic diagram of a control terminal for controlling a wireless remote control aircraft.
Description of reference numerals:
1. a main control module; 2. a sensor module; 21. an angular velocity sensor; 22. an acceleration sensor; 23. A distance sensor; 3. a positioning module; 31. GPS positioning; 32. beidou positioning; 4. an acquisition module; 41. a vision module; 42. a voice module; 5. a wireless communication module; 6. a fan control module; 7. an intelligent terminal; 8. and a power supply module.
Detailed Description
In order to make the technical solutions better understood by those skilled in the art, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only partial embodiments of the present application, but not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
It should be noted that the terms "first," "second," and the like in the description and claims of this application and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It should be understood that the data so used may be interchanged under appropriate circumstances such that embodiments of the application described herein may be used. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
Moreover, some of the above terms may be used to indicate other meanings besides the orientation or positional relationship, for example, the term "on" may also be used to indicate some kind of attachment or connection relationship in some cases. The specific meaning of these terms in the present invention can be understood by those of ordinary skill in the art as appropriate.
Furthermore, the terms "mounted," "disposed," "provided," "connected," and "sleeved" are to be construed broadly. For example, it may be a fixed connection, a removable connection, or a unitary construction; can be a mechanical connection, or an electrical connection; may be directly connected, or indirectly connected through intervening media, or may be in internal communication between two devices, elements or components. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.
As shown in fig. 1, the present application relates to a control terminal for controlling a wireless remote-controlled aircraft, the apparatus comprising: the system comprises a main control module 1, a sensor module 2, a positioning module 3, an acquisition module 4, a wireless communication module 5, a fan control module 6 and an intelligent terminal 7; the sensor module 2 is connected with the main control module 1, the main control module 1 is connected with the positioning module 3, the acquisition module 4, the wireless communication module 5 and the fan control module 6, and the wireless communication module is connected with the intelligent terminal 7;
the sensor module 2 includes: the device comprises an angular velocity sensor 21, an acceleration sensor 22 and a distance sensor 23, wherein the angular velocity sensor 21, the acceleration sensor 22 and the distance sensor 23 are arranged on the aircraft; the acquisition module 4 includes: the vision module 41 and the voice module 42, the vision module 41 is arranged on the aircraft, and the voice module 42 is arranged on the control terminal; the main control module 1 is used for sending control signals to control the sensor module 2, the positioning module 3, the acquisition module 4, the wireless communication module 5 and the fan control module 6 to act; the wireless communication module is used for transmitting a wireless signal to the intelligent terminal 7; the intelligent terminal 7 includes: the intelligent mobile phone APP comprises a smart mobile phone APP, a computer client and an LED display screen, and is used for receiving signals.
Specifically, the main control module 1 is an operation controller for controlling the actions of other modules; the sensor module 2 is used for acquiring information through an induction element, so that the effect of collecting information can be realized; the positioning module 3 is a module capable of realizing a positioning function, so that an accurate positioning effect is realized; the acquisition module 4 is a module for acquiring information and can realize the effect of information acquisition; the wireless communication module 5 is a communication mode of modulating sound, characters, data, images and other electrical signals to be transmitted on radio waves and transmitting the signals to the other party through space and the ground, and a communication mode of transmitting information in the space by using the radio electromagnetic waves is utilized, so that the wireless communication module can be more convenient, more efficient and preferable, can be one or more of WIFI, ZigBee, Bluetooth and RFID, can be suitable for various networks, improves the network compatibility of the system and meets the diversified requirements of users; the fan control module 6 can realize the effect of controlling the direction of the aircraft; the intelligent terminal 7 can be a tablet personal computer or a smart phone, preferably a smart phone, application software pre-installed on the smart phone is APP software, and the state of the monitoring aircraft can be found at any time through the APP software;
the sensor module 2 is connected with the main control module 1, the main control module 1 is connected with the positioning module 3, the acquisition module 4, the wireless communication module 5 and the fan control module 6, the wireless communication module is connected with the intelligent terminal 7, and the main control module 1 is connected with other modules, so that the signal transmission effect can be realized; the sensor module 2 includes: the aircraft control system comprises an angular velocity sensor 21, an acceleration sensor 22 and a distance sensor 23, wherein the angular velocity sensor 21, the acceleration sensor 22 and the distance sensor 23 are arranged on an aircraft and can acquire and feed back data parameters of angular velocity, acceleration and distance, so that the aircraft can be better controlled;
the acquisition module 4 includes: the system comprises a vision module 41 and a voice module 42, wherein the vision module 41 is arranged on the aircraft, and the voice module 42 is arranged on a control terminal and can perform the effect of real-time data feedback; the main control module 1 is used for sending control signals to control the sensor module 2, the positioning module 3, the acquisition module 4, the wireless communication module 5 and the fan control module 6 to act, and the effect of controlling the other modules to act normally can be achieved; the wireless communication module is used for transmitting a wireless signal to the intelligent terminal 7; the intelligent terminal 7 includes: the intelligent mobile phone APP comprises a smart mobile phone APP, a computer client and an LED display screen, and is used for receiving signals.
From the above description, it can be seen that the following technical effects are achieved by the present application:
in the embodiment of the application, adopt the mode of host system 1 wireless control, through being connected sensor module 2 with host system 1, host system 1 and orientation module 3, collection module 4, wireless communication module 5 and fan control module 6 are connected, wireless communication module is connected with intelligent terminal 7, wireless control's purpose has been reached, thereby realized the technical effect that the control degree of difficulty is low and the simple operation, and then solved and adopted a plurality of rockers to input flight control instruction, and because user and unmanned vehicles are the separation in physics, the control degree of difficulty is high and complex operation's technical problem.
Preferably, in this embodiment, the method further includes: and the power supply module 8 is electrically connected with the main control module 1. Through being provided with power module 8, can provide the power to ensure the effect of part normal operating.
Preferably, in this embodiment, the power module 8 is a solar panel. Clean energy, can realize the effect of circulation electricity generation.
Preferably, in this embodiment, the vision module 41 is a high-definition camera. The effect that the video is clear and convenient to identify can be ensured.
Preferably, the model of the high-definition camera is TC-NC9010S 2-MP. Can realize the effect of multiple functions.
Preferably, in this embodiment, the model number of the main control module 1 is STC90C52 AD. The effect of the overall coordinated operation of the aircraft can be realized.
As preferred in this embodiment, the positioning module 3 is a GPS positioning module 31 or a beidou positioning module 32. The effect that the location is accurate and easily realize can be realized.
The above description is only a preferred embodiment of the present application and is not intended to limit the present application, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application.
Claims (8)
1. A control terminal for controlling a wireless remote-controlled aerial vehicle, comprising: the system comprises a main control module, a sensor module, a positioning module, an acquisition module, a wireless communication module, a fan control module and an intelligent end;
the sensor module is connected with the main control module, the main control module is connected with the positioning module, the acquisition module, the wireless communication module and the fan control module, and the wireless communication module is connected with the intelligent terminal;
the sensor module includes: the device comprises an angular velocity sensor, an acceleration sensor and a distance sensor, wherein the angular velocity sensor, the acceleration sensor and the distance sensor are arranged on an aircraft;
the acquisition module comprises: the vision module is arranged on the aircraft, and the voice module is arranged on the control terminal;
the main control module is used for sending control signals to control the sensor module, the positioning module, the acquisition module, the wireless communication module and the fan control module to act;
the wireless communication module is used for transmitting a wireless signal to the intelligent terminal;
the intelligent terminal comprises: the intelligent mobile phone APP comprises a smart mobile phone APP, a computer client and an LED display screen, and is used for receiving signals.
2. The control terminal for controlling a wireless remote-controlled aerial vehicle according to claim 1, characterized by further comprising: and the power supply module is electrically connected with the main control module.
3. A control terminal for controlling a wireless remote control aircraft according to claim 2, wherein the power module is a solar panel.
4. The control terminal for controlling a wireless remote control aircraft according to claim 1, wherein the vision module is a high definition camera.
5. The control terminal for controlling the wireless remote control aircraft according to claim 4, wherein the model of the high-definition camera is TC-NC9010S 2-MP.
6. The control terminal for controlling the wireless remote control aircraft according to claim 1, wherein the wireless communication module is one or more of WIFI, ZigBee, Bluetooth and RFID.
7. The control terminal for controlling a wireless remote-controlled aerial vehicle according to claim 1, wherein the main control module model is STC90C52 AD.
8. The control terminal for controlling the wireless remote control aircraft according to claim 1, wherein the positioning module is a GPS positioning or a beidou positioning.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020880029.4U CN212229451U (en) | 2020-05-23 | 2020-05-23 | Control terminal for controlling wireless remote control aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020880029.4U CN212229451U (en) | 2020-05-23 | 2020-05-23 | Control terminal for controlling wireless remote control aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212229451U true CN212229451U (en) | 2020-12-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020880029.4U Expired - Fee Related CN212229451U (en) | 2020-05-23 | 2020-05-23 | Control terminal for controlling wireless remote control aircraft |
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| Country | Link |
|---|---|
| CN (1) | CN212229451U (en) |
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2020
- 2020-05-23 CN CN202020880029.4U patent/CN212229451U/en not_active Expired - Fee Related
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Granted publication date: 20201225 |