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CN114018245B - Intelligent aiming navigation equipment - Google Patents

Intelligent aiming navigation equipment Download PDF

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Publication number
CN114018245B
CN114018245B CN202111311721.0A CN202111311721A CN114018245B CN 114018245 B CN114018245 B CN 114018245B CN 202111311721 A CN202111311721 A CN 202111311721A CN 114018245 B CN114018245 B CN 114018245B
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CN
China
Prior art keywords
fixedly arranged
navigation
layer frame
motor
base
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Active
Application number
CN202111311721.0A
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Chinese (zh)
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CN114018245A (en
Inventor
刘斐
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Hangzhou Banchi Film and Television Technology Co.,Ltd.
Hangzhou Qibeijia Information Technology Co ltd
Original Assignee
Zhejiang Economic & Trade Polytechnic
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Priority to CN202111311721.0A priority Critical patent/CN114018245B/en
Publication of CN114018245A publication Critical patent/CN114018245A/en
Application granted granted Critical
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C17/00Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/04Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by terrestrial means
    • G01C21/08Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by terrestrial means involving use of the magnetic field of the earth

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)

Abstract

The utility model discloses navigation equipment for photographing view finding points and travel strategies, which relates to the technical field of navigation equipment.

Description

Intelligent aiming navigation equipment
Technical Field
The utility model relates to the technical field of navigation equipment, in particular to intelligent aiming navigation equipment.
Background
What is essential for people to travel is a navigation device, which has changed from simple maps to current electronic products. The electronic product with the display screen is powerful and easy to operate, but is not easy to carry and place when being used outdoors, so that great inconvenience is caused to users, and the electronic product with the display screen is extremely easy to damage when being used outdoors, finally cannot be used, and normal travel of the users is affected.
The utility model of China patent publication No. CN211147688U discloses a multifunctional navigation device for travel, which can protect a device body from being damaged outdoors, but has the main function of being convenient to carry and place in various environments and can not realize the aim navigation.
Disclosure of Invention
In order to solve the technical problems, the utility model adopts the following technical scheme: the intelligent aiming navigation equipment comprises a base, a laser aiming mechanism, a navigation mechanism, a central processing mechanism, a positioning antenna, a roller seat and a roller, wherein the laser aiming mechanism is fixedly arranged on the base; the space direction navigation assembly comprises a space navigation assembly shell, the space navigation assembly shell is fixedly arranged on the navigation assembly shell, an outer layer frame is fixedly arranged on the space navigation assembly shell, a middle layer frame is rotatably arranged on the outer layer frame, an inner layer frame is rotatably arranged on the middle layer frame, an outer layer magnetic plate is fixedly arranged on the middle layer frame, a Hall sensor I is fixedly arranged on the outer layer frame, a middle layer magnetic plate is fixedly arranged on the inner layer frame, a Hall sensor II is fixedly arranged on the middle layer frame, a contact is fixedly arranged on the middle layer frame, and a motor is fixedly arranged on the inner layer frame.
Further, the motor comprises a stator support, a stator and a rotor, wherein the stator is fixedly arranged on the inner layer frame, the stator support is fixedly arranged on the stator, and the rotor is rotatably arranged on the stator.
Further, the middle layer frame is fixedly provided with a contact.
Further, a storage battery for supplying electric energy to the central processing mechanism is fixedly arranged on the base, and a motor for driving the roller seat to rotate on the base is fixedly arranged on the base.
Further, the laser aiming mechanism comprises a polished rod, the polished rod is fixedly arranged on the base, a screw rod motor is fixedly arranged on the base, a screw rod is fixedly arranged on an output shaft of the screw rod motor, a sliding block is slidably arranged on the polished rod, and the sliding block and the screw rod form threaded fit; the slider is fixedly provided with a torsion motor, the output shaft of the torsion motor is fixedly provided with a pinion, the slider is rotatably provided with a laser sighting device, the laser sighting device is fixedly provided with a large gear, and the large gear and the pinion form gear fit.
Further, a magnet support is fixedly arranged on the navigation mechanism shell, and a magnet is slidably arranged on the magnet support.
Further, a motor for driving the roller to rotate on the roller seat is fixedly arranged on the roller seat.
Further, a horizontal direction navigation component is installed on the spatial direction navigation component.
Further, the horizontal direction navigation assembly comprises a telescopic electric cylinder, the telescopic electric cylinder is fixedly arranged on a space navigation assembly shell, a lifting electric cylinder is fixedly arranged on a telescopic rod of the telescopic electric cylinder, a horizontal navigation assembly shell is fixedly arranged on a telescopic rod of the lifting electric cylinder, a storage battery is fixedly arranged on the horizontal navigation assembly shell, a light-emitting diode is fixedly arranged on the horizontal navigation assembly shell, the light-emitting diode is connected with the storage battery through a main wire, a charge plate is fixedly arranged on the horizontal navigation assembly shell, the charge plate is connected with the storage battery through the main wire, and the charge plate is connected with the light-emitting diode through the main wire; the voltage amplifier is fixedly arranged on the horizontal navigation component shell, the voltmeter is connected with the voltage amplifier through an auxiliary lead, and the voltage amplifier is connected with the charge plate through an auxiliary lead; the horizontal navigation component shell is fixedly provided with a baffle plate, the horizontal navigation component shell is fixedly provided with a magnetic needle seat, and the magnetic needle seat is rotatably provided with a magnetic needle.
Further, the upper layer and the lower layer of the horizontal navigation component shell are separated by the partition plate, glue for fixing the storage battery, the light-emitting diode, the charge plate, the voltage amplifier and the voltmeter is injected into the upper layer, and the lower layer is vacuumized.
Compared with the prior art, the utility model has the beneficial effects that: (1) The utility model is provided with the laser aiming mechanism, which can regulate and control aiming when the obstacle is shielded; (2) The horizontal direction navigation component is arranged, and the deflection direction of the device is judged through the change of the magnetic field of the magnetic needle, so that the navigation is more accurate; (3) The utility model sets the space direction navigation component and sets the navigation function in the other two directions of the navigation direction of the horizontal direction navigation component, thereby realizing the omnibearing navigation of the whole device.
Drawings
FIG. 1 is a schematic view of the whole of the present utility model.
Fig. 2 is a schematic view of a laser sighting mechanism according to the present utility model.
FIG. 3 is a schematic diagram of a navigation mechanism according to the present utility model.
FIG. 4 is an external schematic view of a navigation assembly according to the present utility model.
FIG. 5 is a top view of a horizontal navigation module according to the present utility model.
FIG. 6 is a schematic view of the lower layer of the horizontal navigation module according to the present utility model.
FIG. 7 is a schematic view of a telescopic rod of a horizontal navigation module according to the present utility model.
FIG. 8 is a schematic diagram of a spatial directional navigation assembly according to the present utility model.
FIG. 9 is a schematic diagram of a horizontal navigation module motor according to the present utility model.
Reference numerals: 1-a base; 2-a laser aiming mechanism; 3-a navigation mechanism; 4-a central processing mechanism; 5-positioning an antenna; 6-a roller seat; 7-a roller; 8-a horizontal direction navigation component; 9-a spatial direction navigation component; 10-a stator support; 11-a stator; 12-rotor; 201-polish rod; 202-a screw motor; 203-a torsion motor; 204-pinion; 205-large gear; 206-a laser sight; 207-screw rod; 208-a slider; 301-a navigation mechanism housing; 302-a magnet holder; 303-magnet; 801—a horizontal navigation component housing; 802-storage battery; 803-main wire; 804-light emitting diodes; 805-charge plates; 806-voltmeter; 807-secondary leads; 808-a voltage amplifier; 809—a separator; 810-magnetic needle; 811-a magnetic needle holder; 812-lifting electric cylinder; 813-a telescopic electric cylinder; 901-spatial navigation component housing; 902-an outer frame; 903-middle layer frame; 904-inner layer frame; 905-outer magnetic plate; 906-Hall sensor I; 907-middle layer magnetic plate; 908-Hall sensor II; 909-contacts.
Detailed Description
The technical scheme of the utility model is further described below by the specific embodiments with reference to the accompanying drawings.
Wherein the drawings are for illustrative purposes only and are shown in schematic, non-physical, and not intended to be limiting of the present patent; for the purpose of better illustrating embodiments of the utility model, certain elements of the drawings may be omitted, enlarged or reduced and do not represent the size of the actual product; it will be appreciated by those skilled in the art that certain well-known structures in the drawings and descriptions thereof may be omitted.
Examples: the intelligent aiming navigation device as shown in fig. 1-9 comprises a base 1, a laser aiming mechanism 2, a navigation mechanism 3, a central processing mechanism 4, a positioning antenna 5, a roller seat 6 and a roller 7, wherein the laser aiming mechanism 2 is fixedly arranged on the base 1, the navigation mechanism 3 is fixedly arranged on the base 1, the central processing mechanism 4 is fixedly arranged on the base 1, the positioning antenna 5 is fixedly arranged on the central processing mechanism 4, the roller seat 6 is rotatably arranged on the base 1, and the roller 7 is rotatably arranged on the roller seat 6.
The base 1 is fixedly provided with a storage battery for supplying electric energy to the central processing mechanism 4, and the base 1 is fixedly provided with a motor for driving the roller seat 6 to rotate on the base 1.
The laser aiming mechanism 2 comprises a polished rod 201, wherein the polished rod 201 is fixedly arranged on a base 1, a screw rod motor 202 is fixedly arranged on the base 1, a screw rod 207 is fixedly arranged on an output shaft of the screw rod motor 202, a sliding block 208 is slidably arranged on the polished rod 201, and the sliding block 208 and the screw rod 207 form threaded fit; the slider 208 is fixedly provided with a torsion motor 203, an output shaft of the torsion motor 203 is fixedly provided with a pinion 204, the slider 208 is rotatably provided with a laser sight 206, the laser sight 206 is fixedly provided with a large gear 205, and the large gear 205 and the pinion 204 form gear fit. The screw motor 202 is started to drive the screw 207 to rotate, the screw 207 rotates to drive the sliding block 208 to move up and down, and when the sight encounters obstacle shielding, the vertical height of the laser sight 206 is adjusted, so that the sight is convenient to aim at a high place; the torsion motor 203 is started to drive the pinion 204 to rotate, the pinion 204 rotates to drive the large gear 205 to rotate, the large gear 205 rotates to drive the laser sight 206 to rotate, and the angle of the laser sight 206 is adjusted for aiming.
The navigation mechanism 3 comprises a navigation mechanism housing 301, the navigation mechanism housing 301 is fixedly arranged on the base 1, a magnet bracket 302 is fixedly arranged on the navigation mechanism housing 301, a magnet 303 is slidably arranged on the magnet bracket 302, and the magnet 303 slides on the magnet bracket 302 for calibrating the device.
The roller seat 6 is fixedly provided with a motor for driving the roller 7 to rotate on the roller seat 6.
The navigation mechanism housing 301 is fixedly provided with a spatial direction navigation module 9.
The spatial direction navigation module 9 includes a spatial navigation module housing 901, the spatial navigation module housing 901 is fixedly mounted on the navigation mechanism housing 301, an outer frame 902 is fixedly mounted on the spatial navigation module housing 901, a middle frame 903 is rotatably mounted on the outer frame 902, an inner frame 904 is rotatably mounted on the middle frame 903, an outer magnetic plate 905 is fixedly mounted on the middle frame 903, a hall sensor i 906 is fixedly mounted on the outer frame 902, a middle magnetic plate 907 is fixedly mounted on the inner frame 904, a hall sensor ii 908 is fixedly mounted on the middle frame 903, a contact 909 is fixedly mounted on the middle frame 903, and a motor is fixedly mounted on the inner frame 904. When the motor rotates, the shaft of the motor always points to the initial position, and is matched with laser aiming to guide the direction, the middle layer frame 903 rotates on the outer layer frame 902 to drive the outer layer magnetic plate 905 to rotate, the Hall sensor I906 detects the deflection angle of the outer layer magnetic plate 905 to detect the deflection angle of the shaft of the middle layer frame 903, the inner layer frame 904 rotates on the middle layer frame 903 to drive the middle layer magnetic plate 907 to rotate, and the Hall sensor II 908 detects the deflection angle of the middle layer magnetic plate 907 to detect the deflection angle of the shaft of the inner layer frame 904.
The motor includes: the stator support 10, the stator 11 and the rotor 12, wherein the stator 11 is fixedly arranged on the inner layer frame 904, the stator support 10 is fixedly arranged on the stator 11, and the rotor 12 is rotatably arranged on the stator 11.
The middle frame 903 has contacts 909 fixedly mounted thereon. The contact 909 is connected to a power source to provide power to the hall sensor ii 908 on the middle frame 903.
The spatial direction navigation module 9 is provided with a horizontal direction navigation module 8.
The horizontal direction navigation assembly 8 comprises a telescopic electric cylinder 813, the telescopic electric cylinder 813 is fixedly arranged on a space navigation assembly shell 901, a lifting electric cylinder 812 is fixedly arranged on a telescopic rod of the telescopic electric cylinder 813, a horizontal navigation assembly shell 801 is fixedly arranged on a telescopic rod of the lifting electric cylinder 812, a storage battery 802 is fixedly arranged on the horizontal navigation assembly shell 801, a light emitting diode 804 is fixedly arranged on the horizontal navigation assembly shell 801, the light emitting diode 804 is connected with the storage battery 802 through a main wire 803, a charge plate 805 is fixedly arranged on the horizontal navigation assembly shell 801, the charge plate 805 is connected with the storage battery 802 through the main wire 803, and the charge plate 805 is connected with the light emitting diode 804 through the main wire 803; a voltage amplifier 808 is fixedly arranged on the horizontal navigation assembly housing 801, a voltmeter 806 is fixedly arranged on the horizontal navigation assembly housing 801, the voltmeter 806 is connected with the voltage amplifier 808 through a secondary conductor 807, and the voltage amplifier 808 is connected with a charge plate 805 through the secondary conductor 807; a partition 809 is fixedly arranged on the horizontal navigation assembly housing 801, a magnetic needle seat 811 is fixedly arranged on the horizontal navigation assembly housing 801, and a magnetic needle 810 is rotatably arranged on the magnetic needle seat 811. The magnetic field generated by the magnetic needle 810 passes through the charge plate 805, and electrons are deflected to one side due to lorentz force in the magnetic field, at this time, a potential difference is generated between the upper plate and the lower plate of the charge plate 805, the voltage is amplified by the voltage amplifier 808 and transmitted to the voltmeter 806, and the deflection direction of the device can be judged by displaying the numerical value on the voltmeter 806. The lifting electric cylinder 812 stretches and contracts the telescopic rod, the height of the horizontal navigation assembly housing 801 is changed, the telescopic electric cylinder 813 stretches and contracts the telescopic rod, and the front and rear positions of the horizontal navigation assembly housing 801 are changed.
The spacer 809 separates the upper and lower layers of the horizontal navigational assembly housing 801, the upper layer being filled with glue for securing the battery 802, the light emitting diode 804, the charge plate 805, the voltage amplifier 808, the voltmeter 806, and the lower layer being evacuated.

Claims (8)

1. The utility model provides an intelligent aiming navigation equipment, including base (1), laser aiming mechanism (2), navigation mechanism (3), central processing unit (4), positioning antenna (5), gyro wheel seat (6), gyro wheel (7), laser aiming mechanism (2) fixed mounting is on base (1), navigation mechanism (3) fixed mounting is on base (1), central processing unit (4) fixed mounting is on base (1), positioning antenna (5) fixed mounting is on central processing unit (4), gyro wheel seat (6) are rotated and are installed on base (1), gyro wheel (7) are rotated and are installed on gyro wheel seat (6), its characterized in that:
the navigation mechanism (3) comprises a navigation mechanism shell (301), and the navigation mechanism shell (301) is fixedly arranged on the base (1);
a space direction navigation assembly (9) is fixedly arranged on a navigation mechanism shell (301), the space direction navigation assembly (9) comprises a space navigation assembly shell (901), the space navigation assembly shell (901) is fixedly arranged on the navigation mechanism shell (301), an outer layer frame (902) is fixedly arranged on the space navigation assembly shell (901), a middle layer frame (903) is rotatably arranged on the outer layer frame (902), an inner layer frame (904) is rotatably arranged on the middle layer frame (903), an outer layer magnetic plate (905) is fixedly arranged on the middle layer frame (903), a Hall sensor I (906) is fixedly arranged on the outer layer frame (902), a middle layer magnetic plate (907) is fixedly arranged on the inner layer frame (904), a Hall sensor II (908) is fixedly arranged on the middle layer frame (903), a contact (909) is fixedly arranged on the middle layer frame (903), and a motor is fixedly arranged on the inner layer frame (904);
when the motor rotates, the shaft of the motor always points to the initial position, and is matched with laser aiming to guide the direction, the middle layer frame (903) rotates on the outer layer frame (902) to drive the outer layer magnetic plate (905) to rotate, the Hall sensor I (906) detects the deflection angle of the outer layer magnetic plate (905) so as to detect the deflection angle of the shaft of the middle layer frame (903), the inner layer frame (904) rotates on the middle layer frame (903) to drive the middle layer magnetic plate (907) to rotate, and the Hall sensor II (908) detects the deflection angle of the middle layer magnetic plate (907) so as to detect the deflection angle of the shaft of the inner layer frame (904);
the laser aiming mechanism (2) comprises a polished rod (201), wherein the polished rod (201) is fixedly arranged on the base (1), a screw rod motor (202) is fixedly arranged on the base (1), a screw rod (207) is fixedly arranged on an output shaft of the screw rod motor (202), a sliding block (208) is slidably arranged on the polished rod (201), and the sliding block (208) and the screw rod (207) form threaded fit; a torsion motor (203) is fixedly arranged on the sliding block (208), a pinion (204) is fixedly arranged on an output shaft of the torsion motor (203), a laser sighting device (206) is rotatably arranged on the sliding block (208), a large gear (205) is fixedly arranged on the laser sighting device (206), and the large gear (205) and the pinion (204) form gear fit; the screw motor (202) is started to drive the screw (207) to rotate, the screw (207) rotates to drive the sliding block (208) to move up and down, and when the sight encounters obstacle shielding, the vertical height of the laser sight (206) is adjusted, so that the sight is convenient to aim at a high place; the torsion motor (203) is started to drive the pinion (204) to rotate, the pinion (204) rotates to drive the large gear (205) to rotate, the large gear (205) rotates to drive the laser sight (206) to rotate, and the angle of the laser sight (206) is adjusted;
the contact (909) is connected to a power source to supply power to the hall sensor ii (908) on the middle frame (903).
2. An intelligent aiming navigation device according to claim 1, wherein: the motor comprises a stator support (10), a stator (11) and a rotor (12), wherein the stator (11) is fixedly arranged on an inner layer frame (904), the stator support (10) is fixedly arranged on the stator (11), and the rotor (12) is rotatably arranged on the stator (11).
3. An intelligent aiming navigation device according to claim 1, wherein: the base (1) is fixedly provided with a storage battery for providing electric energy for the central processing mechanism (4), and the base (1) is fixedly provided with a motor for driving the roller seat (6) to rotate on the base (1).
4. An intelligent aiming navigation device according to claim 1, wherein: a magnet bracket (302) is fixedly arranged on the navigation mechanism shell (301), and a magnet (303) is slidably arranged on the magnet bracket (302).
5. An intelligent aiming navigation device according to claim 1, wherein: the roller seat (6) is fixedly provided with a motor for driving the roller (7) to rotate on the roller seat (6).
6. An intelligent aiming navigation device according to claim 1, wherein: the space direction navigation component (9) is provided with a horizontal direction navigation component (8).
7. The intelligent aiming navigation device of claim 6, wherein: the horizontal direction navigation assembly (8) comprises a telescopic electric cylinder (813), the telescopic electric cylinder (813) is fixedly arranged on a space navigation assembly shell (901), a lifting electric cylinder (812) is fixedly arranged on a telescopic rod of the telescopic electric cylinder (813), a horizontal navigation assembly shell (801) is fixedly arranged on the telescopic rod of the lifting electric cylinder (812), a storage battery (802) is fixedly arranged on the horizontal navigation assembly shell (801), a light-emitting diode (804) is fixedly arranged on the horizontal navigation assembly shell (801), the light-emitting diode (804) is connected with the storage battery (802) through a main wire (803), a charge plate (805) is fixedly arranged on the horizontal navigation assembly shell (801), the charge plate (805) is connected with the storage battery (802) through the main wire (803), and the charge plate (805) is connected with the light-emitting diode (804) through the main wire (803); a voltage amplifier (808) is fixedly arranged on the horizontal navigation assembly shell (801), a voltmeter (806) is fixedly arranged on the horizontal navigation assembly shell (801), the voltmeter (806) is connected with the voltage amplifier (808) through a secondary lead (807), and the voltage amplifier (808) is connected with a charge plate (805) through the secondary lead (807); a partition board (809) is fixedly arranged on the horizontal navigation assembly housing (801), a magnetic needle seat (811) is fixedly arranged on the horizontal navigation assembly housing (801), and a magnetic needle (810) is rotatably arranged on the magnetic needle seat (811).
8. The intelligent aiming navigation device of claim 7, wherein: the upper layer and the lower layer of the horizontal navigation component shell (801) are separated by a separator (809), glue for fixing the storage battery (802), the light-emitting diode (804), the charge plate (805), the voltage amplifier (808) and the voltmeter (806) is injected into the upper layer, and the lower layer is vacuumized.
CN202111311721.0A 2021-11-08 2021-11-08 Intelligent aiming navigation equipment Active CN114018245B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111311721.0A CN114018245B (en) 2021-11-08 2021-11-08 Intelligent aiming navigation equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111311721.0A CN114018245B (en) 2021-11-08 2021-11-08 Intelligent aiming navigation equipment

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Publication Number Publication Date
CN114018245A CN114018245A (en) 2022-02-08
CN114018245B true CN114018245B (en) 2023-09-15

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Application Number Title Priority Date Filing Date
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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1102084A2 (en) * 1999-11-15 2001-05-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method to determine the orientation of the azimuth direction of a navigation apparatus
CN106679645A (en) * 2016-08-24 2017-05-17 大连理工大学 Real-time navigation device based on multi-directional polarized light
CN209326671U (en) * 2018-10-13 2019-08-30 北京长峰海维电子技术研究所 One kind three is axial to emulate rotation or revolution mechanism for testing without magnetic
CN110657809A (en) * 2019-09-12 2020-01-07 中国人民解放军战略支援部队航天工程大学 Hall sensor installation method for magnetically suspended control sensitive gyroscope
CN111237399A (en) * 2019-08-14 2020-06-05 深圳市智擎新创科技有限公司 Servo steering engine capable of outputting high-precision position information

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1102084A2 (en) * 1999-11-15 2001-05-23 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method to determine the orientation of the azimuth direction of a navigation apparatus
CN106679645A (en) * 2016-08-24 2017-05-17 大连理工大学 Real-time navigation device based on multi-directional polarized light
CN209326671U (en) * 2018-10-13 2019-08-30 北京长峰海维电子技术研究所 One kind three is axial to emulate rotation or revolution mechanism for testing without magnetic
CN111237399A (en) * 2019-08-14 2020-06-05 深圳市智擎新创科技有限公司 Servo steering engine capable of outputting high-precision position information
CN110657809A (en) * 2019-09-12 2020-01-07 中国人民解放军战略支援部队航天工程大学 Hall sensor installation method for magnetically suspended control sensitive gyroscope

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Effective date of registration: 20231116

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