CN106200418B - A kind of TT&C system discrete output signal conditioning circuit - Google Patents
A kind of TT&C system discrete output signal conditioning circuit Download PDFInfo
- Publication number
- CN106200418B CN106200418B CN201610681771.0A CN201610681771A CN106200418B CN 106200418 B CN106200418 B CN 106200418B CN 201610681771 A CN201610681771 A CN 201610681771A CN 106200418 B CN106200418 B CN 106200418B
- Authority
- CN
- China
- Prior art keywords
- stitch
- mouth
- signal
- output signal
- discrete
- 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.)
- Active
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B17/00—Systems involving the use of models or simulators of said systems
- G05B17/02—Systems involving the use of models or simulators of said systems electric
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0208—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the configuration of the monitoring system
- G05B23/0213—Modular or universal configuration of the monitoring system, e.g. monitoring system having modules that may be combined to build monitoring program; monitoring system that can be applied to legacy systems; adaptable monitoring system; using different communication protocols
Abstract
The invention belongs to emulation technologies, and in particular to a kind of TT&C system discrete output signal conditioning module is improved for the emulation to TT&C system emulation platform discrete output signal.When the discrete signal that traditional TT&C system exports external sensor is acquired, since discrete signal type and characteristic are different, need for various types of signal behavior difference discrete magnitude output board cards.The present invention proposes a kind of TT&C system discrete output signal conditioning module, and the standard 5V Transistor-Transistor Logic level that board in TT&C system exports is converted to different types of discrete output signal.Discrete magnitude signal emulation demand, acquires for flight-control computer when meeting flight control system test.
Description
Technical field
The invention belongs to emulation technologies, and in particular to a kind of TT&C system discrete output signal conditioning module, for survey
The emulation for controlling system simulation platform discrete output signal improves.
Background technique
The present invention derives from the testing requirement of flight control system.When testing flight-control computer, observing and controlling system
System needs to emulate the discrete magnitude signal of external sensor output.Including: ground/open, 27V/, 15V/, 27V/ open,
15V/ is opened.
When the discrete signal that traditional TT&C system exports external sensor is acquired, due to discrete signal type and
Characteristic is different, needs for various types of signal behavior difference discrete magnitude output board cards.This mode increases test macro
Complexity and cost.
Summary of the invention
The technical problems to be solved by the present invention are: proposing a kind of TT&C system discrete output signal conditioning module, will survey
The standard 5V Transistor-Transistor Logic level that board exports in control system is converted to different types of discrete output signal.To meet control system of flying
Discrete magnitude signal emulates demand when unified test tries, and acquires for flight-control computer.
TT&C system discrete output signal conditioning module of the invention, the standard 5V TTL electricity for exporting TT&C system
Heibei provincial opera reason is that flight control computer required analog signal, conditioning module input terminal in test are connect by resistance R1 all the way
Ground, another way are connect by NOT gate U1 with the end coil a of relay U2, and the end coil b of relay U2 and external power supply Vcc connect
It connects, common end COM is connect as output port, normal-closed end NC with the second stitch of wire jumper mouth U3, normally open end NO and wire jumper mouth U4
The first stitch connection, wire jumper mouth U4 the second stitch ground connection;The first stitch and third stitch of the wire jumper mouth U3 is distinguished
It is connect with voltage transformation module U5 and voltage transformation module U6.
When desired signal is "/open ", the first stitch and the second stitch of tie jumper mouth U4;When desired signal is
" V1/ " when, the first stitch and the second stitch of tie jumper mouth U4, the first stitch and the second stitch of tie jumper mouth U3;
When desired signal is " V2/ ", the first stitch and the second stitch of tie jumper mouth U4, the second stitch of tie jumper mouth U3
With third stitch;When desired signal is " V1/ is opened ", the first stitch and the second stitch of tie jumper mouth U3;Work as desired signal
When for " V2/ being opened ", the second stitch and third stitch of tie jumper mouth U3.
Protection diode D1 is connected between NOT gate U1 and external power supply Vcc.
The beneficial effects of the present invention are: by this conditioning module, can be greatly decreased testing system board card type class, reduce at
This.
Detailed description of the invention
Fig. 1 is circuit diagram of the invention.
Specific embodiment
The present invention is described in further details below.Referring to Fig. 1,
A kind of TT&C system discrete output signal conditioning module, the standard 5V TTL level for exporting TT&C system
Conditioning is that flight control computer required analog signal, conditioning module input terminal in test are connect by resistance R1 all the way
Ground, another way are connect by NOT gate U1 with the end coil a of relay U2, the end coil b of relay U2 and external power supply Vcc
Connection, common end COM are connect as output port, normal-closed end NC with the second stitch of wire jumper mouth U3, normally open end NO and wire jumper mouth
The first stitch of U4 connects, the second stitch ground connection of wire jumper mouth U4;The first stitch and third stitch point of the wire jumper mouth U3
It is not connect with voltage transformation module U5 and voltage transformation module U6.
When desired signal is "/open ", the first stitch and the second stitch of tie jumper mouth U4;When desired signal is
" V1/ " when, the first stitch and the second stitch of tie jumper mouth U4, the first stitch and the second stitch of tie jumper mouth U3;
When desired signal is " V2/ ", the first stitch and the second stitch of tie jumper mouth U4, the second stitch of tie jumper mouth U3
With third stitch;When desired signal is " V1/ is opened ", the first stitch and the second stitch of tie jumper mouth U3;Work as desired signal
When for " V2/ being opened ", the second stitch and third stitch of tie jumper mouth U3.
Protection diode D1 is connected between NOT gate U1 and external power supply Vcc.
Wherein, when external input standard 5V Transistor-Transistor Logic level signal is high level, signal becomes low level via U1 reverse phase,
And make have voltage on relay U2 coil, and coil attracting electric relay U2 internal switch, the common end COM of relay U2 and normally open end
NO is connected, and for wire jumper mouth U4 by plug jumper cap, can configure signal is earth signal or open circuit signaling, and this signal is sent to 3 ends.
When external input level signal is low level, signal becomes high level via U1 reverse phase, on relay U2 coil
No-voltage, coil are failure to actuate, and relay common end COM and normal-closed end NC are connected, and wire jumper mouth U3 can be matched by plug jumper cap
Confidence number is V1, V2 or open circuit signaling, and this signal is sent to normal-closed end.
In addition, external input power signal VCC can be changed into required voltage V1 by voltage transformation module U5;Voltage transformation module
External input power signal VCC can be changed into required voltage V2 by U6;
It is arranged by wire jumper, realizes the conversion of output signal.By the standard 5V Transistor-Transistor Logic level conversion of board output are as follows: "/
Open ", " V1/ ", " V2/ ", " V1/ is opened ", " V2/ is opened " " opening/ground " signal.
Claims (3)
1. a kind of TT&C system discrete output signal conditioning circuit, the standard 5V Transistor-Transistor Logic level conditioning for exporting TT&C system
For flight control computer in test required analog signal, it is characterised in that: the conditioning module input terminal passes through electricity all the way
R1 ground connection is hindered, another way is connect by NOT gate U1 with the end coil a of relay U2, the end coil b of relay U2 and external electricity
Source Vcc connection, common end COM are connect as output port, normal-closed end NC with the second stitch of wire jumper mouth U3, normally open end NO and jump
The first stitch of line mouth U4 connects, the second stitch ground connection of wire jumper mouth U4;The first stitch and third needle of the wire jumper mouth U3
Foot is connect with voltage transformation module U5 and voltage transformation module U6 respectively.
2. TT&C system discrete output signal conditioning circuit according to claim 1, it is characterised in that: when desired signal is
"/open " when, the first stitch and the second stitch of tie jumper mouth U4;When desired signal is " V1/ ", tie jumper mouth U4
The first stitch and the second stitch, the first stitch and the second stitch of tie jumper mouth U3;When desired signal is " V2/ ",
The first stitch and the second stitch of tie jumper mouth U4, the second stitch and third stitch of tie jumper mouth U3;Work as desired signal
When for " V1/ being opened ", the first stitch and the second stitch of tie jumper mouth U3;When desired signal is " V2/ is opened ", tie jumper mouth
The second stitch and third stitch of U3.
3. TT&C system discrete output signal conditioning circuit according to claim 1 or 2, it is characterised in that: NOT gate U1 with
Protection diode D1 is connected between external power supply Vcc.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610681771.0A CN106200418B (en) | 2016-08-17 | 2016-08-17 | A kind of TT&C system discrete output signal conditioning circuit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201610681771.0A CN106200418B (en) | 2016-08-17 | 2016-08-17 | A kind of TT&C system discrete output signal conditioning circuit |
Publications (2)
Publication Number | Publication Date |
---|---|
CN106200418A CN106200418A (en) | 2016-12-07 |
CN106200418B true CN106200418B (en) | 2019-01-25 |
Family
ID=57522704
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201610681771.0A Active CN106200418B (en) | 2016-08-17 | 2016-08-17 | A kind of TT&C system discrete output signal conditioning circuit |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106200418B (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201893771U (en) * | 2010-11-19 | 2011-07-06 | 陕西千山航空电子有限责任公司 | Universal interface circuit for discrete magnitude acquisition of airborne equipment |
CN102818985A (en) * | 2012-09-10 | 2012-12-12 | 中国航空工业集团公司第六三一研究所 | BIT (Built-In Test) circuit of multipath ground/open discrete magnitude input signal |
CN103684405A (en) * | 2013-11-28 | 2014-03-26 | 陕西千山航空电子有限责任公司 | Discrete signal collection interface |
CN204031119U (en) * | 2014-07-28 | 2014-12-17 | 成都航天通信设备有限责任公司 | Multichannel avionics signals collecting interface circuit |
CN105446318A (en) * | 2015-12-10 | 2016-03-30 | 中国电子科技集团公司第三十二研究所 | Portable measurement and control equipment suitable for carrier rocket flight control system |
-
2016
- 2016-08-17 CN CN201610681771.0A patent/CN106200418B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN201893771U (en) * | 2010-11-19 | 2011-07-06 | 陕西千山航空电子有限责任公司 | Universal interface circuit for discrete magnitude acquisition of airborne equipment |
CN102818985A (en) * | 2012-09-10 | 2012-12-12 | 中国航空工业集团公司第六三一研究所 | BIT (Built-In Test) circuit of multipath ground/open discrete magnitude input signal |
CN103684405A (en) * | 2013-11-28 | 2014-03-26 | 陕西千山航空电子有限责任公司 | Discrete signal collection interface |
CN204031119U (en) * | 2014-07-28 | 2014-12-17 | 成都航天通信设备有限责任公司 | Multichannel avionics signals collecting interface circuit |
CN105446318A (en) * | 2015-12-10 | 2016-03-30 | 中国电子科技集团公司第三十二研究所 | Portable measurement and control equipment suitable for carrier rocket flight control system |
Non-Patent Citations (1)
Title |
---|
"航空离散量输出处理机理及设计实现";蔡叶芳等;《电子技术应用》;20160331;第42卷(第3期);正文第13-15,19页 |
Also Published As
Publication number | Publication date |
---|---|
CN106200418A (en) | 2016-12-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US8582275B2 (en) | Electronic detonator control chip | |
CN104298575B (en) | Mainboard debug circuit | |
CN106208708A (en) | Power supply changeover device and control circuit thereof and standby energy-saving method | |
CN106681302B (en) | The solid-state relay automatic holding device of distribution and its test control method on bullet | |
CN106081046B (en) | A kind of double remaining aerostatics measure and control devices | |
CN102566567A (en) | Electronic control unit (ECU) sensor signal fault injection device for engine hardware in-the-loop simulation (HILS) system | |
CN102608990B (en) | ECU (Electronic Control Unit) actuator control signal fault injection device for engine HILS (Hardware-In-the-Loop Simulation) system | |
CN106200418B (en) | A kind of TT&C system discrete output signal conditioning circuit | |
AU2009242842A1 (en) | An electronic detonator control chip | |
CN209877285U (en) | Circuit for judging running state of compressor | |
CN101131666B (en) | Contact smart card simulation card | |
CN106383479A (en) | Smart cell communication interface compatible circuit, smart cell and unmanned aerial vehicle | |
CN206132974U (en) | Acquisition terminal fault simulating device | |
CN202488384U (en) | Control circuit for soft starter of motor | |
CN108674699A (en) | A kind of satellite equivalent system of the bipolar gating of time-sharing multiplex | |
CN208607547U (en) | Dry contact Peripheral Interface | |
CN106224763A (en) | The monobus control device and method of LNG filling machine multimachine interconnection | |
CN109782660B (en) | Control circuit and device compatible with voltage-type and current-type analog input | |
CN209357053U (en) | A kind of spaceborne relay switch card based on PXI bus testing system | |
CN205489447U (en) | Modular power exports overvoltage protector | |
CN105573513A (en) | Control module for a human-machine dialogue system | |
CN105811951A (en) | Electronic type gantry crane bistable-state switch | |
CN105720957B (en) | Control line power-up state generation circuit | |
CN203554410U (en) | 28V/open circuit discrete magnitude input preprocessing circuit | |
CN109638771A (en) | A kind of application circuit of acceleration transducer in conventional relays protection |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |