CN210521767U

CN210521767U - Four shaft air vehicle based on remote control gloves are controlled

Info

Publication number: CN210521767U
Application number: CN201921089000.8U
Authority: CN
Inventors: 陈超
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-07-11
Filing date: 2019-07-11
Publication date: 2020-05-15
Anticipated expiration: 2029-07-11

Abstract

The utility model discloses a four shaft air vehicle based on remote control gloves are controlled, mainly have four shaft air vehicle, remote controller, the transmitting circuit has on the remote controller, has receiving circuit on the four shaft air vehicle, transmitting circuit contains power module, singlechip, the singlechip disposes transmitting antenna, the singlechip respectively with gravity-feed sensor, button module, voltage detection circuit, light display module connection, power module supplies power for the singlechip after the voltage stabilization processing of boost module, voltage detection circuit is connected with power module; the remote controller is composed of a first assembly and a second assembly, the first assembly is located in the palm of the glove, the second assembly is located on the back of the glove, the four-axis aircraft can run in the swinging direction instantly through gesture swinging, the four-axis aircraft can be driven to do various patterns by combining with function keys at the tiger mouth, and operation is more convenient.

Description

Four shaft air vehicle based on remote control gloves are controlled

Technical Field

The utility model belongs to the technical field of the aircraft toy technique and specifically relates to indicate a four shaft air vehicle based on remote control gloves are controlled.

Background

The quadcopter is also called a quadrotor and a quadrotor helicopter, and is called a quadcopter and a quadrotor for short. The four-axis aircraft is a multi-rotor aircraft, four propellers of the four-axis aircraft are simple mechanisms with directly connected motors, and the cross layout allows the aircraft to obtain the force for rotating the aircraft body by changing the rotating speed of the motors, so that the self posture is adjusted. Present four shaft air vehicle all adopts handheld remote controller to control basically, a plurality of functions and the direction button of distributing on the remote controller, need the operator study and remember the position of button firmly, the side can tentatively control, but because four shaft air vehicle is in the space of four-dimensional activity, it is not easy that the operator will rely on the remote controller to control aerial four shaft air vehicle, direction control error often can appear, the thinking is inconsistent with the operating method the circumstances such as, often the operating error then falls the machine easily, cause the organism to damage, also influence the mood simultaneously.

Disclosure of Invention

The utility model discloses an overcome above-mentioned technical problem, provide a four shaft air vehicle based on remote control gloves is controlled, can operate four shaft air vehicle through the one-hand swing and do the style action, have stronger science and technology and feel.

For solving the above technical problem, the utility model discloses the technical scheme who adopts is:

a four-axis aircraft based on remote control glove control mainly comprises a four-axis aircraft, a remote controller, wherein a transmitting circuit is arranged on the remote controller, a receiving circuit is arranged on the four-axis aircraft, the transmitting circuit comprises a power supply module and a single chip microcomputer, the single chip microcomputer is provided with a transmitting antenna, the single chip microcomputer is respectively connected with a gravity sensing sensor, a button module, a voltage detection circuit and a light display module, the power supply module supplies power to the single chip microcomputer after voltage stabilization processing is carried out on the power supply module through a voltage boosting module, and the voltage detection circuit is connected with the power supply module; the glove is characterized by further comprising a glove, wherein the remote controller is composed of a first assembly and a second assembly, the first assembly is located in the palm of the glove, and the second assembly is located on the back of the glove.

The electric connection line between the first component and the second component is positioned at the mouth of the glove.

The gravity sensing sensor is positioned in the second assembly, one end of the first assembly, which is close to the tiger mouth of the glove, is provided with a function key, and the function key is connected with the key module.

The light display module is positioned in the second component.

The utility model has the advantages that: the novel airplane control mode is provided, single-hand operation is achieved, the direction of the quadcopter can be operated through gesture swing, various pattern actions are achieved through combination of function keys, operation is simpler and more convenient, and playability is strong.

Description of the drawings:

fig. 1 is a layout diagram of a transmission line in the present invention;

fig. 2 is a layout diagram of a receiving circuit in the present invention;

fig. 3 is a schematic structural diagram of the remote controller of the present invention.

In each drawing, a power module 1, a single chip microcomputer 2, a transmitting antenna 3, a gravity sensing sensor 4, a key module 5, a voltage detection circuit 6, a light display module 7, gloves 8, a main control board 10, a boosting module 11, a power supply 20, a gyroscope detection module 30, a barometer detection module 40, a motor drive circuit 50, an electric quantity detection circuit 60, a voltage stabilizing circuit module 70, a first component 81, a second component 82, a receiving antenna 100 and a control light set 200 are connected.

The specific implementation mode is as follows:

the following describes the present invention with reference to the accompanying drawings.

The utility model discloses a four shaft air vehicle based on remote control gloves are controlled, mainly have four shaft air vehicle, remote controller, have transmitting circuit on the remote controller, have receiving circuit on the four shaft air vehicle, as shown in figure 3, still include gloves 8 and gravity induction sensor 4, gloves 8 are cloth gloves, can adopt non-woven fabrics or cotton cloth etc., the remote controller comprises first subassembly 81 and second subassembly 82, first subassembly 81 is located gloves 8 palm, second subassembly 82 is located gloves 8 back, the electric connecting line between first subassembly 81 and second subassembly 82 is located gloves 8 tiger mouth, gravity induction sensor 4 is located second subassembly 82, through left and right rocking, make gravity induction sensor 4 send control signal to receiving circuit through 2, can control aircraft flight direction, the one end that first subassembly 81 is close to gloves 8 tiger mouths has the function key, the function keys are operated by the thumb and connected with the key module 5, and the light display module 7 is positioned in the second assembly 82.

The utility model discloses have aerial mode and secret mode, through the rotational speed of adjusting different motors, can realize multiple aerial flight special effect under the aerial mode, through the configuration pulley, can realize multiple underground under the secret mode and slide the special effect.

As shown in fig. 1, the transmitting circuit is a control circuit of the remote controller, the glove gravity sensing remote controller is adopted, the transmitting circuit comprises a power module 1 and a single chip microcomputer 2, the single chip microcomputer 2 is provided with a transmitting antenna 3, the single chip microcomputer 2 is respectively connected with a gravity sensing sensor 4, a key module 5, a voltage detection circuit 6 and a light display module 7, the power module 1 supplies power to the single chip microcomputer 2 after being subjected to voltage stabilization processing by a boosting module 11, and the voltage detection circuit 6 is connected with the power module 1. The processor of the single chip microcomputer 2 is HW2171B (the main IC and the 2.4GRF are sealed into a whole), the type of the IC adopted by the boost module 11 can be AX2L-3V3, the 3V power supply voltage is stabilized by a voltage stabilizing circuit, the voltage is stabilized at 3.3V and then supplied to the single chip microcomputer 2, and after the function of each function group is started, the single chip microcomputer shapes and amplifies the code signal through the 2.4GRF and then sends the signal to a receiving circuit.

After decoding is completed, the single chip microcomputer 2 simultaneously scans the numerical value fed back by the gravity sensor 4 and the numerical value of the key, the value is assigned and the number is taken after the scanning is completed, the single chip microcomputer 2 is used for solving a signal code and sending the signal code to 2.4G, and then the signal code is sent out. The light display module 7 displays states through LED lamps, and the states are controlled by signals output by the singlechip 2 when the LED lamp is started. The voltage detection circuit 6 always detects the power supply voltage in real time from starting, when the power supply voltage is lower than a certain value, the voltage detection circuit 6 provides the numerical value for the single chip microcomputer 2, the single chip microcomputer 2 outputs a signal to the light display module 7, and then the low-voltage alarm state is displayed through the LED.

Receiving a line: referring to fig. 2, the portable electronic device includes a main control board 10 and a power supply 20, the main control board 10 is provided with a receiving antenna 100, the main control board 10 is respectively connected to a gyroscope detection module 30, a barometer detection module 40, a motor driving circuit 50, and an electric quantity detection circuit 60, and the main control board 10 is connected to a control light set 200. The motor driving circuit respectively controls the first motor, the second motor, the third motor and the fourth motor, the power supply 20 respectively supplies power to the main control board 10, the gyroscope detection module 30 and the barometer detection module 40 through the voltage stabilizing circuit module 70, and the power supply 20 simultaneously supplies power to the motor driving circuit 50.

In this embodiment, the main control board 10 is 2.4GRF + main control MCU, the MCU model can adopt HW2181B, the IC of the voltage stabilizing circuit module 70 can adopt 6206-2.8V, the power voltage of the power supply 20 is 3.7V, the light group 200 adopts an LEDD light bar, the gyroscope detection module 30 is used for converting data collected by a gyroscope, the inclination angle change data of the aircraft is provided, the barometer detection module 40 is used for converting data collected by a barometer, and the aircraft altitude change data is provided.

The working principle of the receiving circuit is as follows:

1. after the whole machine is electrified, voltage stabilization treatment is firstly carried out, and the voltage is stabilized at 2.8V and then supplied to the main control board 10, the gyroscope and the barometer;

2. the 2.4G of the main control board 10 collects the signals sent by the transmitter through the antenna for processing, and then the signals are provided to the main control board 10 for decoding;

3. after decoding, the main control board 10 firstly performs action control on the signals sent by the transmitters, and outputs the signals to the motor driving circuit 50 to respectively control each motor and drive the aircraft to perform action;

4. after the aircraft takes off, the main control board 10 firstly detects the gyroscope and the barometer through the gyroscope detection module 30 and the barometer detection module 40, and compensates according to the state of the gyroscope and the barometer after detection, so that the gyroscope and the barometer are stably suspended in the air;

5. after the flight state is preliminarily finished, the flight action can be carried out according to the signal transmitted by the remote controller.

The flight action of the air mode comprises the following steps: the function keys control correction, unlocking, one-key takeoff, one-key landing, accelerator ascending and descending, low and medium speed switching, front 360-degree rolling, rear 360-degree rolling, headless mode, one-key backward, high-speed rotation, automatic circling, emergency landing, and simple gestures control course left and right turning, forward moving, backward moving, left flying and right flying.

The underground mode is based on the aerial mode, and can operate forward, backward, left-turn and right-turn on the ground by configuring the pulleys.

The four-axis aircraft changes the rotating speed of the flying wing by adjusting the rotating speeds of the four motors, so that the change of the lift force is realized, and the flying posture and the position of the aircraft are controlled.

The utility model discloses a four shaft air vehicle can add the camera, realizes the function of taking photo by plane.

In light of the foregoing description of the preferred embodiments of the present invention, those skilled in the art can make various changes and modifications without departing from the spirit of the present invention. The technical scope of the present invention is not limited to the content of the specification, and must be determined according to the scope of the claims.

Claims

1. The utility model provides a four shaft air vehicle based on remote control gloves are controlled, mainly have four shaft air vehicle, remote controller have transmitting circuit on the remote controller, have receiving circuit on the four shaft air vehicle, its characterized in that: the transmitting circuit comprises a power supply module (1) and a single chip microcomputer (2), the single chip microcomputer (2) is provided with a transmitting antenna (3), the single chip microcomputer (2) is respectively connected with a gravity sensing sensor (4), a key module (5), a voltage detection circuit (6) and a light display module (7), the power supply module (1) supplies power to the single chip microcomputer (2) after voltage stabilization processing through a voltage boosting module (11), and the voltage detection circuit (6) is connected with the power supply module (1); the remote control is characterized by further comprising a glove (8), the remote control is composed of a first assembly (81) and a second assembly (82), the first assembly (81) is located in the palm of the glove (8), and the second assembly (82) is located on the back of the glove (8).

2. The quadcopter based on remote control glove manipulation according to claim 1, wherein: the electrical connection line between the first component (81) and the second component (82) is located at the mouth of the glove (8).

3. A quadcopter based remote glove manipulation according to claim 1 or 2, wherein: the gravity sensing sensor (4) is arranged in the second assembly (82), one end, close to the tiger mouth of the glove (8), of the first assembly (81) is provided with a function key, and the function key is connected with the key module (5).

4. The quadcopter based on remote control glove manipulation according to claim 3, wherein: the light display module (7) is located in the second component (82).