CN112651079A - Angle simulation resolving device for electromechanical airborne product - Google Patents
Angle simulation resolving device for electromechanical airborne product Download PDFInfo
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- CN112651079A CN112651079A CN202011501016.2A CN202011501016A CN112651079A CN 112651079 A CN112651079 A CN 112651079A CN 202011501016 A CN202011501016 A CN 202011501016A CN 112651079 A CN112651079 A CN 112651079A
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- angle
- interface
- angle simulation
- power supply
- control assembly
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- 238000004088 simulation Methods 0.000 title claims abstract description 42
- 238000006243 chemical reaction Methods 0.000 claims description 24
- 230000000087 stabilizing effect Effects 0.000 claims description 12
- 238000004364 calculation method Methods 0.000 claims description 8
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 description 7
- 238000004891 communication Methods 0.000 description 5
- 230000010354 integration Effects 0.000 description 2
- 238000013524 data verification Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/30—Circuit design
Abstract
The angle simulation resolving device for the electromechanical airborne product comprises a case, wherein an angle simulation resolving unit, a control assembly and a switch power supply are arranged in the case, the angle simulation resolving unit is connected with the control assembly, and the switch power supply is respectively connected with the angle simulation resolving unit and the control assembly to provide electric energy for the angle simulation resolving unit and the control assembly; the machine case is provided with a signal interface connected with the angle simulation resolving unit, and the signal interface is used for being connected with an external airborne product; the case is provided with a control interface connected with the control assembly, and the control interface is used for being connected with a computer; the case is provided with a power interface connected with the switching power supply. The device is mainly used for simulating and sending the course, the attitude, the radio and other angle signals of the electromechanical products of the airplane, and simultaneously can receive and solve the course, the attitude, the radio and other angle signals output by the electromechanical products of the airplane.
Description
Technical Field
The invention belongs to the technical field of signal simulation, and particularly relates to an angle simulation resolving device for an electromechanical airborne product.
Background
The airborne product signal simulation is mainly used for simulating and sending the heading, attitude, radio and other angle signals of the electromechanical product of the airplane, and meanwhile, the airborne product signal simulation can receive and solve the heading, attitude, radio and other angle signals output by the electromechanical product of the airplane. The currently used airborne product signal simulation method mostly adopts airborne product pieces to simulate or solve the angle signals of the course, the attitude, the radio and the like of the airplane, and has the advantages of high cost, lower precision, inconvenient use, and poorer integration and expandability. Improvements are therefore proposed.
Disclosure of Invention
The technical problems solved by the invention are as follows: the invention provides an angle simulation resolving device for an electromechanical airborne product, which is mainly used for simulating and sending course, attitude, radio and other angle signals of the electromechanical product of an airplane and receiving and resolving the course, attitude, radio and other angle signals output by the electromechanical product of the airplane.
The technical scheme adopted by the invention is as follows: the angle simulation resolving device for the electromechanical airborne product comprises a case, wherein an angle simulation resolving unit, a control assembly and a switch power supply are arranged in the case, the angle simulation resolving unit is connected with the control assembly, and the switch power supply is respectively connected with the angle simulation resolving unit and the control assembly to provide electric energy for the angle simulation resolving unit and the control assembly; the machine case is provided with a signal interface connected with the angle simulation resolving unit, and the signal interface is used for being connected with an external airborne product; the case is provided with a control interface connected with the control assembly, and the control interface is used for being connected with an external computer; the power supply interface is connected with the switch power supply and used for being connected with commercial power.
The technical scheme is further limited, the control assembly comprises a single chip microcomputer, an interface conversion chip and a voltage stabilizing circuit, the single chip microcomputer is connected and communicated with the angle analog calculation unit through an IO signal port, the single chip microcomputer is connected with the interface conversion chip, the single chip microcomputer realizes transmission of digital signals between the single chip microcomputer and a computer through the interface conversion chip, the voltage stabilizing circuit is connected with the single chip microcomputer and the interface conversion chip, and the switching power supply is connected with the voltage stabilizing circuit and supplies power to the single chip microcomputer and the interface conversion chip through the voltage stabilizing circuit.
In addition, the technical scheme is further limited, and the interface conversion chip adopts a TTL (transistor-transistor logic) serial port conversion chip or a USB (universal serial bus) serial port conversion chip.
In order to further limit the technical scheme, the angle simulation calculating unit adopts a self-adjusting angle or a rotary angle module.
Compared with the prior art, the invention has the advantages that:
the device integrates the angle simulation calculation unit, the control assembly, the switching power supply and various interface components into a case, and has the advantages of high integration degree, compact structure, small volume, low manufacturing cost, high simulation precision, convenience in use and easiness in integrating and expanding angle simulation and calculation of the electromechanical airborne product.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the 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 invention.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation. The use of the phrase "comprising one of the elements" does not exclude the presence of other like elements in the process, method, article, or apparatus that comprises the element.
Referring to fig. 1, an embodiment of the present invention is described in detail.
An angle simulation resolving device for electromechanical airborne products, as shown in fig. 1, including quick-witted case 1, machine case 1 is inside to be equipped with angle simulation resolving unit 2, control assembly 3 and switching power supply 11, angle simulation resolving unit 2 is connected with control assembly 3, switching power supply 11 is connected with angle simulation resolving unit 2 and control assembly 3 respectively and provides the electric energy for it. The machine case 1 is provided with a signal interface 9 connected with the angle simulation resolving unit 2, and the signal interface 9 is used for being connected with an external airborne product 10; the case 1 is provided with a control interface 7 connected with the control component 3, and the control interface 7 is used for being connected with an external computer 8; the power supply unit comprises a case 1, a switch power supply 11, a power supply interface 12 connected with the switch power supply 11, wherein the power supply interface 12 is used for being connected with a mains supply 13, and the mains supply 13 is AC220 input.
Specifically, the control component 3 includes a single chip 4, an interface conversion chip 5 and a voltage stabilizing circuit 6. The single chip microcomputer 4 is connected with the angle simulation resolving unit 2 for communication through an IO signal port; the single chip microcomputer 4 is connected with an interface conversion chip 5, the single chip microcomputer 4 realizes the transmission of digital signals with a computer 8 through the interface conversion chip 5, and preferably, the interface conversion chip 5 adopts a TTL serial port conversion chip or a USB serial port conversion chip. The voltage stabilizing circuit 6 is connected with the single chip microcomputer 4 and the interface conversion chip 5, and the switching power supply 11 is connected with the voltage stabilizing circuit 6 and supplies power to the single chip microcomputer 4 and the interface conversion chip 5 through the voltage stabilizing circuit 6. The invention adopts the singlechip 4 for control, can realize the communication with an external PC, realize the angle sending control and the angle receiving resolving, realize the communication data verification and data encryption, reduce the communication error rate and ensure the communication data safety.
The angle simulation resolving unit 2 adopts a self-integral angle module or a rotary variable angle module, so that the precision is high, the quality is stable, the highest precision can reach 0.02 degree, and the test requirement of aviation products is met.
The case 1 adopts a 2U 19-inch standard cabinet plug-in box, the control switch and the work indicator light are installed on the front panel of the case 1, and the power supply and the signal line are wired from the rear panel of the case 1.
The connector between each component of the invention is an aviation connector or an industrial connector.
The device can be independently used as an angle sending part and an angle receiving part, and can also be integrated in test equipment to be used as a certain functional unit.
The device is mainly used for simulating and sending the course, the attitude, the radio and other angle signals of the electromechanical product of the airplane, and simultaneously can receive and solve the course, the attitude, the radio and other angle signals output by the electromechanical product of the airplane.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (4)
1. A angle simulation solver for electromechanical machine carries product, including quick-witted case (1), its characterized in that: an angle simulation calculation unit (2), a control assembly (3) and a switching power supply (11) are arranged in the case (1), the angle simulation calculation unit (2) is connected with the control assembly (3), and the switching power supply (11) is respectively connected with the angle simulation calculation unit (2) and the control assembly (3) to provide electric energy for the angle simulation calculation unit (2) and the control assembly (3); the machine case (1) is provided with a signal interface (9) connected with the angle simulation resolving unit (2), and the signal interface (9) is used for being connected with an external airborne product (10); the case (1) is provided with a control interface (7) connected with the control component (3), and the control interface (7) is used for being connected with an external computer (8); the power supply device is characterized in that a power supply interface (12) connected with a switching power supply (11) is arranged on the case (1), and the power supply interface (12) is used for being connected with a mains supply (13).
2. The angle simulation solver for electromechanical on-board products according to claim 1, wherein: the control assembly (3) comprises a single chip microcomputer (4), an interface conversion chip (5) and a voltage stabilizing circuit (6), the single chip microcomputer (4) is connected with the angle simulation calculation unit (2) through an IO signal port and communicates, the single chip microcomputer (4) is connected with the interface conversion chip (5), the single chip microcomputer (4) achieves transmission of digital signals between the single chip microcomputer (4) and the computer (8) through the interface conversion chip (5), the voltage stabilizing circuit (6) is connected with the single chip microcomputer (4) and the interface conversion chip (5), and the switching power supply (11) is connected with the voltage stabilizing circuit (6) and supplies power to the single chip microcomputer (4) and the interface conversion chip (5) through the voltage stabilizing circuit (6).
3. The angle simulation solver for electromechanical on-board products according to claim 2, wherein: the interface conversion chip (5) adopts a TTL serial port conversion chip or a USB serial port conversion chip.
4. The angle simulation solver for electromechanical on-board products according to claim 1, wherein: the angle simulation resolving unit (2) adopts a self-integer angle module or a rotary variable angle module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011501016.2A CN112651079A (en) | 2020-12-17 | 2020-12-17 | Angle simulation resolving device for electromechanical airborne product |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011501016.2A CN112651079A (en) | 2020-12-17 | 2020-12-17 | Angle simulation resolving device for electromechanical airborne product |
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| CN112651079A true CN112651079A (en) | 2021-04-13 |
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| CN202011501016.2A Pending CN112651079A (en) | 2020-12-17 | 2020-12-17 | Angle simulation resolving device for electromechanical airborne product |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070243505A1 (en) * | 2006-04-13 | 2007-10-18 | Honeywell International Inc. | System and method for the testing of air vehicles |
| CN103744064A (en) * | 2013-12-18 | 2014-04-23 | 中国人民解放军海军航空工程学院青岛校区 | Airborne weather radar attitude signal simulator and simulation test method |
| CN105000194A (en) * | 2015-08-13 | 2015-10-28 | 史彩成 | UAV (unmanned aerial vehicle) assisted landing visual guiding method and airborne system based on ground cooperative mark |
| CN207595296U (en) * | 2017-10-16 | 2018-07-10 | 陕西特恩电子科技有限公司 | A kind of integrated test system |
| US20190249992A1 (en) * | 2017-06-06 | 2019-08-15 | Clearpath Robotics Inc. | Systems and methods for electronic mapping and localization within a facility |
| CN209842389U (en) * | 2019-07-22 | 2019-12-24 | 中国人民解放军空军工程大学航空机务士官学校 | Airplane radio compass signal simulator |
| CN210479069U (en) * | 2019-09-20 | 2020-05-08 | 中国人民解放军海军航空大学 | Aircraft attitude and heading test system |
-
2020
- 2020-12-17 CN CN202011501016.2A patent/CN112651079A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070243505A1 (en) * | 2006-04-13 | 2007-10-18 | Honeywell International Inc. | System and method for the testing of air vehicles |
| CN103744064A (en) * | 2013-12-18 | 2014-04-23 | 中国人民解放军海军航空工程学院青岛校区 | Airborne weather radar attitude signal simulator and simulation test method |
| CN105000194A (en) * | 2015-08-13 | 2015-10-28 | 史彩成 | UAV (unmanned aerial vehicle) assisted landing visual guiding method and airborne system based on ground cooperative mark |
| US20190249992A1 (en) * | 2017-06-06 | 2019-08-15 | Clearpath Robotics Inc. | Systems and methods for electronic mapping and localization within a facility |
| CN207595296U (en) * | 2017-10-16 | 2018-07-10 | 陕西特恩电子科技有限公司 | A kind of integrated test system |
| CN209842389U (en) * | 2019-07-22 | 2019-12-24 | 中国人民解放军空军工程大学航空机务士官学校 | Airplane radio compass signal simulator |
| CN210479069U (en) * | 2019-09-20 | 2020-05-08 | 中国人民解放军海军航空大学 | Aircraft attitude and heading test system |
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