CN202720319U - A debugging device of an electric servo mechanism - Google Patents
A debugging device of an electric servo mechanism Download PDFInfo
- Publication number
- CN202720319U CN202720319U CN 201220341365 CN201220341365U CN202720319U CN 202720319 U CN202720319 U CN 202720319U CN 201220341365 CN201220341365 CN 201220341365 CN 201220341365 U CN201220341365 U CN 201220341365U CN 202720319 U CN202720319 U CN 202720319U
- Authority
- CN
- China
- Prior art keywords
- servo mechanism
- electric servo
- electric
- control plane
- debugging
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Abstract
The utility model discloses a debugging device of an electric servo mechanism and belongs to the field of computer application and machinery precision measurement. The debugging device comprises a PC, a PC debugging software, a RS-232 serial cable, a RS-232/422 converter, a dedicated testing cable, an electric servo mechanism, a control plane, and a three coordinate measuring system. When the control portion of the electric servo mechanism is powered on, in accordance with system requirement of the electric servo mechanism, the debugging device of the electric servo mechanism transmits an error amplification coefficient, a feedforward amplification coefficient, a feedback amplification coefficient and control signal, and a current sensor deviation signal to the electric servo mechanism through software and the communication cable, and all the signals are saved in a memory unit of the electric servo mechanism. According to the machinery zero setting requirement of the system control plane, the control plane deflection modification value measured by the three coordinate measuring system is saved in the memory unit of the electric servo mechanism so as to guarantee the zero position of control plane within the required ranged of the electric servo mechanism.
Description
Technical field
The utility model relates to a kind of electric servomechanism, computer communication, and mechanical precision measurement belongs to computer utility and mechanical precision measurement field, is used for the debugging of digitalized electric servo control mechanism.
Background technology
Aircraft generally is comprised of analog device with the electric servomechanism control section, has the characteristics of debug difficulties; In recent years, along with the development of integrated circuit, the development of electric digital servo control mechanism is very fast, but the model of electric digital servo control mechanism is different, and debugging does not also have a kind of suitable device.
The utility model content
Technical problem to be solved in the utility model provides a kind of electric servomechanism debugging apparatus, and this device has easy to use, and it is convenient to debug, and satisfies the characteristics of small space rudder face zeroing.
For solving the problems of the technologies described above, electric servomechanism debugging apparatus of the present utility model is characterised in that, comprises computing machine, RS-232 serial cable, RS-232/RS-422 converter, special test cable; Described computing machine connects the RS-232/RS-422 converter by described RS-232 serial cable, and described RS-232/RS-422 converter connects described special test cable, and described special test cable connects electric servomechanism, and described electric servomechanism connects rudder face.
For carrying out the zero-bit debugging of rudder face, further, the utility model also comprises the three-coordinates measuring machine of measuring position, rudder face angle, and described three-coordinates measuring machine connects rudder face on the one hand, is electrically connected on the other hand described electric servomechanism.
The utlity model has easy to usely, it is convenient to debug, and satisfies the characteristics of small space rudder face zeroing, can improve the debugging efficiency of digital servomechanism, solves the rudder face zeroing problem of small space.
Description of drawings
Fig. 1 is the structured flowchart of electric servomechanism debugging apparatus.
Embodiment
As shown in Figure 1, computing machine connects the RS-232/RS-422 converter by the RS-232 serial cable, and the RS-232/RS-422 converter connects electric servomechanism by the special test cable, and electric servomechanism connects rudder face.Three-coordinates measuring machine connects rudder face on the one hand, is electrically connected on the other hand described electric servomechanism.Installation and Debugging software in the computing machine contains communication and data storing software in the digitalized electric servo control mechanism.
The course of work of the present utility model is as follows: press accompanying drawing 1 and connect the electric servomechanism debugging apparatus, when the energising of digitalized electric servo control mechanism control section, software enters after the bookbinding subroutine, start the debugging software on the computing machine, click " connection " button, setting up the electric servomechanism debugging software is connected with the communication of electric servomechanism bookbinding software, according to the electric servomechanism system requirements, the error originated from input amplification coefficient, the feedforward amplification coefficient, the feedback amplification coefficient, current amplification factor, according to digitalized electric servo control mechanism institute observing and controlling signal processed, the current sensor deviation, input correction of deviation coefficient, click " bookbinding ", set each coefficient is passed to the digitalized electric servo control mechanism with parameter, and is stored in the digitalized electric servo control mechanism memory by bitcom.Each parameter of system and non-once are given just to meet the demands, and needs repeatedly to adjust, and this electric servomechanism debugging apparatus can be realized repeatedly binding, and satisfies the system debug demand.
Rudder face zero-bit debug process of the present utility model is as follows: press accompanying drawing 1 and connect the electric servomechanism debugging apparatus, the energising of digitalized electric servo control mechanism, drift angle with the relative mechanical zero of three-coordinates measuring machine test servo control mechanism amount rudder face, gained drift angle dress is changed to respective digital amount in the digitalized electric servo control mechanism, by servo control mechanism debugging apparatus software, the angle of rudder reflection modified value is bound into digitalized electric servo control mechanism memory cell.This debug process has solved the problem that small space rudder face zero-bit can't be adjusted in the system, has satisfied the commissioning requirements of system.
It should be noted last that, above embodiment is only unrestricted in order to the technical solution of the utility model to be described, those of ordinary skill in the art is to be understood that, can make amendment or be equal to replacement the technical solution of the utility model, and not breaking away from the spirit and scope of technical solutions of the utility model, it all should be encompassed in the middle of the claim scope of the present utility model.
Claims (2)
1. an electric servomechanism debugging apparatus is characterized in that, comprises computing machine, RS-232 serial cable, RS-232/RS-422 converter, special test cable; Described computing machine connects the RS-232/RS-422 converter by described RS-232 serial cable, and described RS-232/RS-422 converter connects described special test cable, and described special test cable connects electric servomechanism, and described electric servomechanism connects rudder face.
2. a kind of electric servomechanism debugging apparatus according to claim 1 is characterized in that, also comprises the three-coordinates measuring machine of measuring position, rudder face angle, and described three-coordinates measuring machine connects rudder face on the one hand, is electrically connected on the other hand described electric servomechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220341365 CN202720319U (en) | 2012-07-13 | 2012-07-13 | A debugging device of an electric servo mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220341365 CN202720319U (en) | 2012-07-13 | 2012-07-13 | A debugging device of an electric servo mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202720319U true CN202720319U (en) | 2013-02-06 |
Family
ID=47622141
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220341365 Expired - Lifetime CN202720319U (en) | 2012-07-13 | 2012-07-13 | A debugging device of an electric servo mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202720319U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104198103A (en) * | 2014-09-12 | 2014-12-10 | 北京新立机械有限责任公司 | On-line real-time measurement system for precision assembly |
| CN104654933A (en) * | 2015-03-12 | 2015-05-27 | 上海新跃仪表厂 | Electric servo mechanism and debugging method thereof |
| CN108466704A (en) * | 2018-03-23 | 2018-08-31 | 四川瑞航电子科技有限公司 | A kind of aircraft rudder surface measuring system and its measurement method |
| CN112526877A (en) * | 2020-11-06 | 2021-03-19 | 北京精密机电控制设备研究所 | Servo system debugging method and device |
| CN113252353A (en) * | 2021-04-06 | 2021-08-13 | 浙江蓝箭航天空间科技有限公司 | Horizontal test method for electromechanical servo mechanism of carrier rocket and computer storage medium |
-
2012
- 2012-07-13 CN CN 201220341365 patent/CN202720319U/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104198103A (en) * | 2014-09-12 | 2014-12-10 | 北京新立机械有限责任公司 | On-line real-time measurement system for precision assembly |
| CN104654933A (en) * | 2015-03-12 | 2015-05-27 | 上海新跃仪表厂 | Electric servo mechanism and debugging method thereof |
| CN104654933B (en) * | 2015-03-12 | 2016-06-01 | 上海新跃仪表厂 | A kind of electric servomechanism and adjustment method thereof |
| CN108466704A (en) * | 2018-03-23 | 2018-08-31 | 四川瑞航电子科技有限公司 | A kind of aircraft rudder surface measuring system and its measurement method |
| CN112526877A (en) * | 2020-11-06 | 2021-03-19 | 北京精密机电控制设备研究所 | Servo system debugging method and device |
| CN112526877B (en) * | 2020-11-06 | 2023-11-14 | 北京精密机电控制设备研究所 | Servo system debugging method and device |
| CN113252353A (en) * | 2021-04-06 | 2021-08-13 | 浙江蓝箭航天空间科技有限公司 | Horizontal test method for electromechanical servo mechanism of carrier rocket and computer storage medium |
| CN113252353B (en) * | 2021-04-06 | 2023-09-22 | 浙江蓝箭航天空间科技有限公司 | Carrier rocket electromechanical servo mechanism horizontal test method and computer storage medium |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202720319U (en) | A debugging device of an electric servo mechanism | |
| CN201574786U (en) | Servomotor digitalized servo system of steam turbine unit | |
| CN204883407U (en) | Servo pressure control system | |
| CN104483650A (en) | Calibration method for ammeter | |
| CN101863140A (en) | Slide block pressure and speed display and control system of hydraulic press for powder products | |
| CN205300929U (en) | Simulate electric main shaft reliability test device of sound attitude cutting force on line | |
| CN201477170U (en) | Transient power quality quick detection device | |
| CN104991582A (en) | Servo pressure control system | |
| CN211653115U (en) | Automatic calibration system for digital current sensor | |
| CN202024750U (en) | Environmental temperature protection device and three coordinate measuring machine | |
| CN204716668U (en) | Servovalve detection device in a kind of Hydrauservo System | |
| CN103900742B (en) | Pressure unit | |
| CN203657964U (en) | Pressure transmitter | |
| CN202550969U (en) | Two-way digital proportional valve amplifier | |
| CN102689185A (en) | Combination machine for riveting cylinder gasket | |
| CN205175583U (en) | Sensor temperature compensation circuit | |
| CN209261973U (en) | Digital hydraulic servo control device | |
| CN202711000U (en) | Three-dimensional high-precision full-automatic ultra-high frequency band radar antenna near-field test closed-loop control system | |
| CN210719210U (en) | Multi-channel proximity sensor digital resolving module | |
| CN206230415U (en) | A kind of servomotor automatic positioning equipment | |
| CN202815509U (en) | Precision positioning device capable of eliminating backlash error by utilizing error correction closed loop | |
| CN204883211U (en) | Automatic excitation control unit of calibration function | |
| CN202814620U (en) | Separated type pressure sensor | |
| CN203787239U (en) | Exhaust temperature meter compensation adjusting resistor box | |
| CN202267557U (en) | Full automatic torque repeating offset measuring system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130206 |