CN105739386B - A kind of airborne school flies the implementation method of remote monitoring system - Google Patents
A kind of airborne school flies the implementation method of remote monitoring system Download PDFInfo
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- CN105739386B CN105739386B CN201610136551.XA CN201610136551A CN105739386B CN 105739386 B CN105739386 B CN 105739386B CN 201610136551 A CN201610136551 A CN 201610136551A CN 105739386 B CN105739386 B CN 105739386B
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- cooperative target
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Classifications
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- 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
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0423—Input/output
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- 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
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/25—Pc structure of the system
- G05B2219/25449—Constructive details
Abstract
The present invention relates to the implementation method that a kind of airborne school flies remote monitoring system, and on machine or ground sends control instruction, and control cooperative target parameter is changed, the described method comprises the following steps：Step 1: design completes system constructing by controller of embeded processor, safe and reliable control effect is realized；Step 2: design communication frame structure, realizes more cooperative targets, multi-parameter facility control.Remote control to cooperative target on machine can be achieved on ground automatically according to needs in task using the method for the present invention, cost and software development difficulty are low, have extremely strong application value.
Description
Technical field
The present invention relates to the implementation method that a kind of airborne school flies remote monitoring system.Belong to control field of engineering technology.
Background technology
School fly to be flown in desired trajectory using the aircraft for loading cooperative target (answering machine etc.), ground observing and controlling equipment tracking
Cooperative target on aircraft, the aircraft-position information obtained by accuracy evaluation on machine and earth station's tracking parameter are carried out at data
Reason obtains the related system index and performance indications of ground installation, is calculated for the orbit determination in actual combat task.Due to ground installation
System is more, each system operating mode is more, brings cooperative target substantial amounts, mode parameter control is complicated, and school flies inherently
It is that a costly engineering is tired out, it is necessary to make full use of the effective flight time to obtain the flying quality of maximum for data
Product.In this case it is necessary to design a kind of remote monitoring system, can be needed according to ground observing and controlling equipment to cooperative target on machine
Mark is controlled.
In December, 2008《Remote measuring and controlling》6th phase paper《School based on Modbus agreements flies centralized monitoring system》Disclose
A kind of school flies the design method of centralized monitoring system, and this method integrated application Modbus field bus techniques are soft with reference to KingView
Part feature, construct school and fly centralized monitoring system.The monitoring system of the winged equipment in airborne school is developed using KingView, realizes machine
Carry real-time monitoring, control that school flies equipment.
In October, 2008《Remote measuring and controlling》5th phase paper《Airborne school flies the design and emulation of monitoring system》Disclose one kind
Airborne school flies the design method of monitoring system, and this method has carried out detailed design to the soft and hardware of system, and in Proteus
Emulated, by building virtual environment, complete software levels translocation examination.
These research general character advantages are for aircraft model feature, with reference to cooperative target control characteristic, are made full use of existing
The advantage of technology, comprehensive various mature technologies, completes Project design or emulation.These systems are using notebook as control
Potential safety hazard be present in device, its lithium battery；Manual operation is needed on aircraft, instruction will issue navigator from earth station by short-wave radio set
Member, navigator are notifying operator to carry out correlation, and not only realtime control can not ensure, and be operated on machine under vibration environment
Safety can not also ensure；Control of the system to cooperative target is complicated, and link is more, causes security of system to reduce.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of airborne school for above-mentioned prior art to fly remote monitoring system
The design method of system, system constructing is completed by master-plan, ensured communication safety by design agreement, have that cost is low, work(
The characteristics of energy is strong, favorable expandability.
Technical scheme is used by the present invention solves the above problems：A kind of airborne school flies the realization side of remote monitoring system
Method, on machine or ground sends control instruction, and control cooperative target parameter is changed, the described method comprises the following steps：
The first step, by controller of embeded processor system constructing is completed, realize safe and reliable control
System uses three class control strategy, specially boat-carrying side controller, airborne two neck controller and airborne bomb bay control
Device processed, boat-carrying side controller are made up of embedded controller and data radio station, for remotely sending and receiving control instruction, are easy to
Cooperative target state on understanding machine；Airborne two neck controllers and bomb bay controller are placed on diverse location on machine, airborne two neck
Controller is positioned over second navigator position, for passing through embedded controller emergency operation cooperative target, bomb bay controller
Bomb bay is placed on cooperative target, is made up of embedded controller, data radio station and I/O modules, used for system debug,
Controlled with the information exchange and cooperative target of boat-carrying side controller, wherein being adopted between airborne two neck controller and bomb bay controller
Connected with RS485 buses, connection is realized using penetrating cable on machine；Bomb bay controller is adopted with cooperative target and I/O modules
With network connection, it is easy to centralized Control and system to extend；
Second step, design communication frame structure, realize more cooperative targets, multi parameters control
Frame method is compiled using selection and carries out communication frame structure design, communication frame structure is specially：Answering machine address is 1byte's
Device address, multiple answering machines number from 01-FF；The control model that model selection is 1byte selects, including 01 pattern
Equipment power up down control and 02 pattern answering machine state modulator；Control content is divided into power up down control and state modulator,
Power up down control represents that power-up, 00 represent to power off with 01, and state modulator includes parameter and numerical value, and multiple parameters are according to parameter+number
Value is arranged in order；CRC check is 2byte CRC check value, and for guaranteeing data security, the parsing of communication frame structure is placed on fried
In internal weapon bays controller, specific analysis mode is is described using ini file, when cooperative target etc. changes, by more
Change ini file content, control logic can be achieved without other changes.
Compared with prior art, the advantage of the invention is that：
(1) system design that the present invention designs has inexpensive feature.
(2) frame format that the present invention designs has flexible feature.
(3) present invention takes into account the design problem for considering system extension.
Brief description of the drawings
Fig. 1 is the flow chart for the implementation method that a kind of airborne school of the present invention flies remote monitoring system.
Fig. 2 is systematic schematic diagram in a kind of implementation method of the winged remote monitoring system in airborne school of the present invention.
Fig. 3 is communication frame schematic diagram in a kind of implementation method of the winged remote monitoring system in airborne school of the present invention.
Fig. 4 is frame assumption diagram in a kind of implementation method of the winged remote monitoring system in airborne school of the present invention.
Embodiment
The present invention is described in further detail below in conjunction with accompanying drawing embodiment.
The present invention relates to the implementation method that a kind of airborne school flies remote monitoring system, and on machine or ground sends control and referred to
Order, control cooperative target parameter are changed, and solve the requirement of collection different mode data as needed, specific as shown in Figure 1
Process is：
The first step, using embeded processor as controller complete system constructing, realize safe and reliable control effect
According to multiple the cooperative target power up down and state modulator target of system design, system uses three class control strategy,
Specially boat-carrying side controller, airborne two neck controller and airborne bomb bay controller, boat-carrying side controller is by embedded Control
Device and data radio station composition, for remotely sending and receiving control instruction, are easy to cooperative target state on understanding machine；Airborne two neck
Controller and bomb bay controller are placed on diverse location on machine, and airborne two necks controller is positioned over second navigator position, used
In by embedded controller emergency operation cooperative target, bomb bay controller is placed on bomb bay with cooperative target, by being embedded in
Formula controller, data radio station and ADAM-6000 modules (the I/O modules of China being ground, for control device power up down) composition, are used for
System debug is used, controlled with the information exchange of boat-carrying side controller and cooperative target, and the block diagram of system is as shown in Figure 2.
Due to environment special on machine, controller uses two kinds of interface shapes of RS485 buses and network, wherein it is airborne two neck controller and
RS485 buses are used between bomb bay controller, connection is realized using penetrating cable on machine；Bomb bay controller and cooperative target with
And I/O modules etc. use network connection, it is easy to centralized Control and system to extend.Embedded primary processor is using Samsung
S3C2416ARM926, Systematic selection wince, convenient download can be realized using C#, the multithreading that has, multitask, completely
The characteristics of preemptive type.Airborne bomb bay controller is that system controls performer, and receiving instruction includes airborne two necks controller, ship
Carrying side controller or the machine produces, instruction includes ON/OFF instruction, state modulator instruction, after ON/OFF instruction is received, control
The break-make that ADAM-6000 modules correspond to I/O ports realizes the power up down of cooperative target；After state modulator instruction is received, composition
Cooperative target information frame, control cooperative target action, whole system design is clear, reasonable, and interface specification, control is simple, cost
It is cheap.
Second step, design communication frame structure, realize more cooperative targets, multi-parameter facility control
Just because of use controlled in wireless and three class control strategy, and data radio station is also RS485 communication modes, and is closed
Make in target control containing classified informations such as frequencies, it is necessary to design a kind of communication frame to ensure the safety of small data, large information capacity
Reliable interaction, frame method is compiled using selection here and is designed.It is based on cooperative target control parameter accurately understand based on, and
And these parameters have various selectable item, carry out custom coding to these options to realize, the principle of frame method is compiled in selection
As shown in Figure 3.According to principle, the frame format of design as shown in figure 4, answering machine address is 1byte device address, to it is multiple should
Machine is answered number from 01-FF；The control model that model selection is 1byte selects, and includes the equipment power up down control of 01 pattern
With the answering machine state modulator of 02 pattern；Control content is divided into power up down control and state modulator, power up down 01 table of control
Show that power-up, 00 represent power-off, state modulator includes parameter (parameter of each answering machine is numbered according to 01-FF) and numerical value
(selectable value of each parameter is numbered according to 01-FF), multiple parameters are arranged in order according to parameter+numerical value；CRC check is
2byte CRC check value, for guaranteeing data security, such as control 2# answering machines the 3rd parameter (selectable value 1,15,
50) 50, the 4th parameters (selectable value 0.3,1.5,2.0) are set to and are set to 1.5, then frame is written as 02 (address 02) 02 (pattern
For state modulator) 03 (the 3rd parameter) 03 (the 3rd numerical value) 04 (the 4th parameter) 02 (the 2nd numerical value) XXXX (CRC check).
The parsing of frame structure is placed in bomb bay controller, and specific analysis mode is is described using ini file, in cooperative target etc.
When changing, by changing ini file content, control logic can be achieved without other changes, it is seen that the compact spirit of frame structure
Living, versatility is very strong.
In addition to the implementation, it is all to use equivalent transformation or equivalent replacement present invention additionally comprises there is other embodiment
The technical scheme that mode is formed, it all should fall within the scope of the hereto appended claims.
Claims (2)
1. a kind of airborne school flies the implementation method of remote monitoring system, on machine or ground sends control instruction, controls cooperative target
Mark parameter is changed, it is characterised in that：It the described method comprises the following steps：
The first step, by controller of embeded processor system constructing is completed, realize safe and reliable control
System uses three class control strategy, specially boat-carrying side controller, airborne two neck controller and airborne bomb bay controller,
Boat-carrying side controller is made up of embedded controller and data radio station, for remotely sending and receiving control instruction, is easy to understand
Cooperative target state on machine；Airborne two neck controller and airborne bomb bay controller are placed on diverse location on machine, airborne two neck
Controller is positioned over second navigator position, for passing through embedded controller emergency operation cooperative target, airborne bomb bay control
Device processed is placed on bomb bay with cooperative target, is made up of embedded controller, data radio station and I/O modules, for system debug
Using, control with the information exchange of boat-carrying side controller and cooperative target, wherein airborne two neck controller and airborne bomb bay
Connected between controller using RS485 buses, connection is realized using penetrating cable on machine；Airborne bomb bay controller and cooperative target
And I/O modules use network connection, it is easy to centralized Control and system to extend；
Second step, design communication frame structure, realize more cooperative targets, multi parameters control
Frame method is compiled using selection and carries out communication frame structure design, communication frame structure is specially：Cooperative target address is setting for 1byte
Standby address, multiple cooperative targets number from 01-FF；The control model that model selection is 1byte selects, including 01 pattern
Cooperative target power up down control and 02 pattern cooperative target state modulator；Control content is divided into power up down control and parameter
Control, power up down control represent that power-up, 00 represent to power off with 01, and state modulator includes parameter and numerical value, and multiple parameters are according to ginseng
Number+numerical value is arranged in order；CRC check is 2byte CRC check value, and for guaranteeing data security, the parsing of communication frame structure is put
In airborne bomb bay controller, specific analysis mode is is described using ini file, when cooperative target changes,
By changing ini file content, control logic can be achieved without other changes.
2. a kind of airborne school according to claim 1 flies the implementation method of remote monitoring system, it is characterised in that：The conjunction
It is answering machine to make target.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610136551.XA CN105739386B (en) | 2016-02-28 | 2016-02-28 | A kind of airborne school flies the implementation method of remote monitoring system |
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| CN201610136551.XA CN105739386B (en) | 2016-02-28 | 2016-02-28 | A kind of airborne school flies the implementation method of remote monitoring system |
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| CN105739386A CN105739386A (en) | 2016-07-06 |
| CN105739386B true CN105739386B (en) | 2018-04-06 |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107483476B (en) * | 2017-09-07 | 2020-05-22 | 中国人民解放军63686部队 | Method for realizing control of cooperative target in flight correction route |
| CN112947266B (en) * | 2021-04-30 | 2021-09-28 | 江苏航运职业技术学院 | Remote monitoring communication method and system for ship power device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201229400Y (en) * | 2007-12-17 | 2009-04-29 | 张万松 | Aeroplane answering machine landing system utilizing S-mode answering machine |
| CN101694753A (en) * | 2009-10-15 | 2010-04-14 | 四川九洲电器集团有限责任公司 | Information transmission system, information transmission device and information transmission method |
| CN104569944A (en) * | 2014-12-26 | 2015-04-29 | 中国民用航空华东地区空中交通管理局安徽分局 | Radar flight inspection result analysis system |
| CN204945370U (en) * | 2015-09-29 | 2016-01-06 | 四川天中星航空科技有限公司 | Answering machine detection system |
| CN105222807A (en) * | 2015-10-14 | 2016-01-06 | 中国民航大学 | A kind of rotor wing unmanned aerial vehicle precision approach path indicator check system and method for calibration |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6640560B2 (en) * | 2001-06-07 | 2003-11-04 | Hamilton Sundstrand | Distributed electronic control for air conditioning system |
| US7240879B1 (en) * | 2005-05-06 | 2007-07-10 | United States of America as represented by the Administration of the National Aeronautics and Space Administration | Method and associated apparatus for capturing, servicing and de-orbiting earth satellites using robotics |
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201229400Y (en) * | 2007-12-17 | 2009-04-29 | 张万松 | Aeroplane answering machine landing system utilizing S-mode answering machine |
| CN101694753A (en) * | 2009-10-15 | 2010-04-14 | 四川九洲电器集团有限责任公司 | Information transmission system, information transmission device and information transmission method |
| CN104569944A (en) * | 2014-12-26 | 2015-04-29 | 中国民用航空华东地区空中交通管理局安徽分局 | Radar flight inspection result analysis system |
| CN204945370U (en) * | 2015-09-29 | 2016-01-06 | 四川天中星航空科技有限公司 | Answering machine detection system |
| CN105222807A (en) * | 2015-10-14 | 2016-01-06 | 中国民航大学 | A kind of rotor wing unmanned aerial vehicle precision approach path indicator check system and method for calibration |
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| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Li Pei Inventor after: Xia Lili Inventor after: Zhou Jinbiao Inventor after: Pan Gaofeng Inventor after: Shi Zhaofan Inventor after: Su Inventor after: Ji Yuanxin Inventor after: Liu Sifang Inventor after: Xie Yong Inventor after: Xue Jun Inventor before: Li Pei Inventor before: Pan Gaofeng Inventor before: Su Inventor before: Ji Yuanxin Inventor before: Xie Yong Inventor before: Xue Jun Inventor before: Xia Lili Inventor before: Wang Shaolin |
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Granted publication date: 20180406 Termination date: 20190228 |