CN111459180A - Gesture-controlled airplane - Google Patents

Gesture-controlled airplane Download PDF

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Publication number
CN111459180A
CN111459180A CN202010138083.6A CN202010138083A CN111459180A CN 111459180 A CN111459180 A CN 111459180A CN 202010138083 A CN202010138083 A CN 202010138083A CN 111459180 A CN111459180 A CN 111459180A
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CN
China
Prior art keywords
lateral wall
gesture
block
side wall
control block
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Pending
Application number
CN202010138083.6A
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Chinese (zh)
Inventor
程煜
朱才智
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Shenzhen Octant Technology Co ltd
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Shenzhen Octant Technology Co ltd
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Publication date
Application filed by Shenzhen Octant Technology Co ltd filed Critical Shenzhen Octant Technology Co ltd
Priority to CN202010138083.6A priority Critical patent/CN111459180A/en
Publication of CN111459180A publication Critical patent/CN111459180A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Toys (AREA)

Abstract

The invention provides a gesture-controlled airplane, which relates to the technical field of unmanned aerial vehicles and comprises a buffer block and a wrist strap, wherein a receiving device is arranged on the side wall of one end of the buffer block, the receiving device comprises a control block, the side wall of one end of a control machine is fixedly connected with the side wall of one end of the buffer block, a processing chip, a power supply interface and a first 2.4G module are sequentially and fixedly connected into the inner cavity of the buffer block, a power supply is inserted into the side wall of one end of the control block, the output end of the power supply is inserted into the power supply interface and abuts against the inner wall of the power supply interface, a power device is arranged on the side wall of one side of the control block, a control device is arranged on. Controlling means and receiving arrangement use and fly the operation through wrist strap control unmanned aerial vehicle, avoid the tradition need use the remote controller when operation unmanned aerial vehicle flies, complex operation, the device's the easy-to-use nature of effective improve equipment of application.

Description

Gesture-controlled airplane
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a gesture-controlled airplane.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
But most unmanned aerial vehicles now need use the remote controller to control in operation process, and complex operation influences the use, need improve.
Disclosure of Invention
The invention aims to solve the defects in the prior art and provides a gesture-controlled airplane.
In order to achieve the purpose, the invention adopts the following technical scheme: the utility model provides an aircraft of gesture control, includes buffer block and wrist strap, the one end lateral wall of buffer block is provided with receiving arrangement, receiving arrangement includes the control block, the one end lateral wall of controller and the one end lateral wall fixed connection of buffer block, the inner chamber of buffer block fixedly connected with in proper order handles chip, power supply interface and first 2.4G module, the one end lateral wall of control block is inserted and is equipped with the power, the output of power inserts power supply interface and offsets rather than the inner wall, a lateral wall of control block is provided with power device, a lateral wall of wrist strap is provided with controlling means.
The power device comprises a plurality of supports, one side wall of each support is fixedly connected with one side wall of the control block, one end side wall of each support is fixedly connected with a motor, and a driving end of each motor is sleeved with a rotating blade and fixedly connected with the rotating blade.
The control device comprises a protection block, one side wall of the protection block is fixedly connected with one side wall of the wrist strap, and the inner cavity of the protection block is sequentially and fixedly connected with a second 2.4G module, an optical flow module, a gyroscope and a battery.
The number of the supports is four, the supports are arranged at equal intervals, the supports are made of carbon fiber composite materials through pressing and cutting, and the strength of the supports is enhanced.
The control block is the square, one side lateral wall of control block adopts the fillet to handle, one side lateral wall of control block adopts abrasive paper to polish and handles, improve equipment's pleasing to the eye degree.
The side wall of one end of the motor is fixedly connected with the side wall of one end of the support through bolts, and the rotating speed of the motor is 8070r/min, so that the normal operation of the equipment is ensured.
Advantageous effects
1. According to the invention, the control device and the receiving device are adopted, and the unmanned aerial vehicle is controlled by the wrist strap to carry out flight operation, so that the problem that a remote controller is required to be used when the unmanned aerial vehicle is operated to fly in the traditional method, the operation is complex, and the device is applied to effectively improve the usability of the equipment.
Drawings
FIG. 1 is a front view of a gesture controlled aircraft according to the present invention;
FIG. 2 is a bottom view of a gesture controlled aircraft according to the present invention;
FIG. 3 is a schematic structural diagram of a receiving device in an airplane controlled by gestures according to the present invention;
fig. 4 is a schematic structural diagram of a control device in an airplane controlled by gestures according to the present invention.
Illustration of the drawings: 1. a receiving device; 11. a control block; 12. a first 2.4G module; 13. a power supply interface; 14. processing the chip; 2. a power plant; 21. a support; 22. rotating the leaves; 23. a motor; 3. a wristband; 4. a control device; 41. a protection block; 42. a battery; 43. a gyroscope; 44. an optical flow module; 45. a second 2.4G module; 5. a buffer block; 6. a power source.
Detailed Description
In order to make the technical means, the original characteristics, the achieved purposes and the effects of the invention easily understood, the invention is further described below with reference to the specific embodiments and the attached drawings, but the following embodiments are only the preferred embodiments of the invention, and not all embodiments. Based on the embodiments in the implementation, other embodiments obtained by those skilled in the art without any creative efforts belong to the protection scope of the present invention.
Specific embodiments of the present invention are described below with reference to the accompanying drawings.
The specific embodiment is as follows:
referring to fig. 1-4, a gesture-controlled airplane comprises a buffer block 5 and a wrist strap 3, wherein a receiving device 1 is arranged on one side wall of the buffer block 5, the receiving device 1 comprises a control block 11, the control block 11 is a cube, one side wall of the control block 11 is processed by a fillet, one side wall of the control block 11 is polished by abrasive paper, the attractiveness of the airplane is improved, one side wall of a controller is fixedly connected with one side wall of the buffer block 5, a processing chip 14, a power supply interface 13 and a first 2.4G module 12 are sequentially and fixedly connected to an inner cavity of the buffer block 5, a power supply 6 is inserted into one side wall of the control block 11, an output end of the power supply 6 is inserted into the power supply interface 13 and abuts against the inner wall of the power supply, a power device 2 is arranged on one side wall of the control block 11, the power device 2 comprises a plurality of supports 21, support 21 adopts carbon-fibre composite to suppress and tailor and makes, strengthen support 21's intensity, one side lateral wall of support 21 and one side lateral wall fixed connection of control block 11, the one end lateral wall fixed connection of support 21 has motor 23, adopt bolt fixed connection between the one end lateral wall of motor 23 and the one end lateral wall of support 21, the rotational speed of motor 23 is 8070r/min, guarantee the normal operating of equipment, the drive end cover of motor 23 is established and fixedly connected with commentaries on classics leaf 22, one side lateral wall of wrist strap 3 is provided with controlling means 4, be convenient for drive equipment operation.
Controlling means 4 includes protection piece 41, one side lateral wall of protection piece 41 and one side lateral wall fixed connection of wrist strap 3, the inner chamber of protection piece 41 is fixedly connected with second 2.4G module 45 in proper order, light stream module 44, gyroscope 43 and battery 42, through setting up controlling means 4 and receiving arrangement 1, the use is carried out the flight operation through 3 control unmanned aerial vehicle of wrist strap, avoid the tradition need use the remote controller when operation unmanned aerial vehicle flies, complex operation, the device's the effective improve equipment's of application ease for use.
The working principle of the invention is as follows: when using, insert power supply interface 13 with power 6, the unmanned aerial vehicle power supply, control command is sent out to the bracelet and gives 2.4G module, and the bracelet passes through gyroscope 43 and detects the acceleration in the six directions of 3 axles, because horizontal low-speed motion is difficult to detect, so including light stream module 44, calculate speed, draw eight instructions that horizontal flight starts, the palm level keeps the wrist motionless, and the bracelet does not send any instruction this moment, rises: slowly lifting the palm; stopping rising: the palm is pressed down quickly; and (3) descending: the palm is lifted downwards slowly; stopping descending: the palm is lifted up quickly; flying left: the palm moves left slowly; stopping left flight: the palm moves right quickly; and (3) flying to the right: the palm moves to the right slowly; stopping right flight: the palm moves left quickly; forward flying, namely, the palm moves forwards slowly; and (3) forward stopping: the palm moves backwards quickly; backward flying, namely, slowly moving the palm backward; and (3) backing and stopping: the palm moves forward quickly; landing, namely landing through a button of the bracelet, and detecting that the ground is stopped; the machine automatically stops when contacting the ground by gesture descending; when the self horizontal attitude angle exceeds 90 degrees, the machine is automatically stopped; the vertical direction then detects with the acceleration, can obtain 4 instructions, through setting up controlling means 4 and receiving arrangement 1, uses and carries out the flight operation through 3 control unmanned aerial vehicle of wrist strap, avoids the tradition to need to use the remote controller when operation unmanned aerial vehicle flies, complex operation, the device's the easy-to-use nature of effective improve equipment of application.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (8)

1. A gesture-controlled aircraft comprising a buffer block (5) and a wrist strap (3), characterized in that: the utility model discloses a damping device, including buffer block (5), receiving arrangement (1), control block (11), the one end lateral wall of controller and the one end lateral wall fixed connection of buffer block (5), the inner chamber of buffer block (5) is fixedly connected with in proper order handles chip (14), power supply interface (13) and first 2.4G module (12), the one end lateral wall of control block (11) is inserted and is equipped with power (6), the output of power (6) inserts power supply interface (13) and offsets rather than the inner wall, a lateral wall of control block (11) is provided with power device (2), a lateral wall of wrist strap (3) is provided with controlling means (4).
2. A gesture-controlled aircraft according to claim 1, wherein: power device (2) include a plurality of supports (21), one side lateral wall of support (21) and one side lateral wall fixed connection of control block (11), the one end lateral wall fixed connection of support (21) has motor (23), the drive end cover of motor (23) is established and fixedly connected with commentaries on classics leaf (22).
3. A gesture-controlled aircraft according to claim 1, wherein: the control device (4) comprises a protection block (41), one side wall of the protection block (41) is fixedly connected with one side wall of the wrist strap (3), and the inner cavity of the protection block (41) is sequentially and fixedly connected with a second 2.4G module (45), an optical flow module (44), a gyroscope (43) and a battery (42).
4. A gesture-controlled aircraft according to claim 2, wherein: the number of the supports (21) is four, and the four supports (21) are arranged at equal intervals.
5. A gesture-controlled aircraft according to claim 1, wherein: the control block (11) is a cube, one side lateral wall of the control block (11) adopts fillet processing, and one side lateral wall of the control block (11) adopts sand paper to polish.
6. A gesture-controlled aircraft according to claim 2, wherein: and the side wall of one end of the motor (23) is fixedly connected with the side wall of one end of the bracket (21) by bolts.
7. A gesture-controlled aircraft according to claim 2, wherein: the rotating speed of the motor (23) is 8070 r/min.
8. A gesture-controlled aircraft according to claim 4, wherein: the support (21) is made of carbon fiber composite materials through pressing and cutting.
CN202010138083.6A 2020-03-03 2020-03-03 Gesture-controlled airplane Pending CN111459180A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010138083.6A CN111459180A (en) 2020-03-03 2020-03-03 Gesture-controlled airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010138083.6A CN111459180A (en) 2020-03-03 2020-03-03 Gesture-controlled airplane

Publications (1)

Publication Number Publication Date
CN111459180A true CN111459180A (en) 2020-07-28

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CN202010138083.6A Pending CN111459180A (en) 2020-03-03 2020-03-03 Gesture-controlled airplane

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105223959A (en) * 2015-09-28 2016-01-06 佛山市南海区广工大数控装备协同创新研究院 A kind of unmanned plane glove control system and control method
CN106094846A (en) * 2016-05-31 2016-11-09 中国航空工业集团公司西安飞机设计研究所 A kind of aircraft flight control methods
CN107831788A (en) * 2017-12-01 2018-03-23 深圳蚁石科技有限公司 A kind of flight control system and control method
CN207718231U (en) * 2018-01-15 2018-08-10 江西理工大学 A kind of gesture identification remote controlled drone
CN209962219U (en) * 2019-08-19 2020-01-17 中北大学 Wearable unmanned aerial vehicle gesture control device
CN210078843U (en) * 2019-06-14 2020-02-18 黄伟光 Four-axis remote control aircraft

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105223959A (en) * 2015-09-28 2016-01-06 佛山市南海区广工大数控装备协同创新研究院 A kind of unmanned plane glove control system and control method
CN106094846A (en) * 2016-05-31 2016-11-09 中国航空工业集团公司西安飞机设计研究所 A kind of aircraft flight control methods
CN107831788A (en) * 2017-12-01 2018-03-23 深圳蚁石科技有限公司 A kind of flight control system and control method
CN207718231U (en) * 2018-01-15 2018-08-10 江西理工大学 A kind of gesture identification remote controlled drone
CN210078843U (en) * 2019-06-14 2020-02-18 黄伟光 Four-axis remote control aircraft
CN209962219U (en) * 2019-08-19 2020-01-17 中北大学 Wearable unmanned aerial vehicle gesture control device

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Application publication date: 20200728

RJ01 Rejection of invention patent application after publication