CN106506032A - A kind of peace control remote measurement integration general module - Google Patents

A kind of peace control remote measurement integration general module Download PDF

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Publication number
CN106506032A
CN106506032A CN201611058920.4A CN201611058920A CN106506032A CN 106506032 A CN106506032 A CN 106506032A CN 201611058920 A CN201611058920 A CN 201611058920A CN 106506032 A CN106506032 A CN 106506032A
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CN
China
Prior art keywords
unit
remote measurement
signal
peace control
amplifier
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.)
Pending
Application number
CN201611058920.4A
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Chinese (zh)
Inventor
姚先秀
马文超
李科连
黄鹤明
唐旭
聂志华
张玉新
聂荣
周曦
周之丽
高茜
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201611058920.4A priority Critical patent/CN106506032A/en
Publication of CN106506032A publication Critical patent/CN106506032A/en
Pending legal-status Critical Current

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    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/38Transceivers, i.e. devices in which transmitter and receiver form a structural unit and in which at least one part is used for functions of transmitting and receiving
    • H04B1/40Circuits
    • GPHYSICS
    • G08SIGNALLING
    • G08CTRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
    • G08C17/00Arrangements for transmitting signals characterised by the use of a wireless electrical link
    • G08C17/02Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Signal Processing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The present invention relates to a kind of peace control remote measurement integration general module, including:L/S dual-band antennas (1), modulation /demodulation module (2), power amplifier components (3), the component that accepts filter (4), transmitting-receiving subassembly (5), remote measurement transmitter unit (6), peace control receiving unit (7), digital units (8), upconverting unit (9), pre-amplifier unit (10), low-noise amplifier (11), mixing filter (12), AGC amplifier (13).The peace control remote measurement integrated module of the present invention, achieve peace control reception antenna and remote measurement transmitting antenna integrated design, circuit miniaturization, there is versatility, reduce design cost simultaneously, various guided missile, the examination of unmanned plane target, batch inspection, the flight parameter collection of war instruction, record and security control demand can be met.

Description

A kind of peace control remote measurement integration general module
Technical field
The invention belongs to guided missile missile-borne or unmanned aerial vehicle onboard peace control, remote-measuring equipment field, and in particular to a kind of peace control remote measurement Integrated general module.
Background technology
Guided missile and unmanned plane are tried, criticize in the flight tests such as inspection, war instruction in target, need to pass through missile-borne or airborne telemetering system is real-time Collection, record guided missile, the running parameter of each system of unmanned plane, are launched to ground control station by wireless communication link, recorded, are shown After showing, store and processing, guided missile service behaviour and each system working regularity in flight test is analyzed;Missile-borne or machine need to be passed through Carry Safety system and receive the safety control command that ground control system sends, complete the security control during guided missile, unmanned plane during flying.
But traditional like product has the following disadvantages:1) it is made up of two autonomous devices of telemetry system and Safety system, Equipment includes telemetry transmetter, power amplifier, remote measurement transmitting antenna, security controlling receiver, peace control reception antenna, apparatus assembly Many, volume is big, high cost;2) telemetry system, Safety system frequency are fixed, bit rate is fixed, communication cycle is fixed, versatility Difference.Therefore, it is badly in need of developing a kind of miniaturization, generalization, modularity, the peace control remote measurement integrated module of low cost, is reducing into In the case of this, various guided missile, the examination of unmanned plane target, batch inspection, the flight parameter collection of war instruction, record and security control need are met Ask.
Content of the invention
The present invention proposes a kind of miniaturization, generalization, modularity, the peace control remote measurement integrated module of low cost, is reducing In the case of cost, various guided missile, the examination of unmanned plane target, batch inspection, the flight parameter collection of war instruction, record and security control need are met Ask.
The problems referred to above of prior art are considered, according to one side disclosed by the invention, the present invention adopts following technology Scheme:
A kind of peace control remote measurement integration general module, including:L/S dual-band antennas (1) and modulation /demodulation module (2);Its In, modulation /demodulation module (2) includes power amplifier components (3), the component that accepts filter (4), transmitting-receiving subassembly (5);Transmitting-receiving subassembly (5) includes Remote measurement transmitter unit (6), peace control receiving unit (7), digital units (8);Remote measurement transmitter unit (6) include upconverting unit (9), Pre-amplifier unit (10);Peace control receiving unit (7) includes low-noise amplifier (11), mixing filter (12), AGC amplifier (13);
Powered to the peace control integrated general module of remote measurement by signal and power supply processing unit, while the flight parameter that will be gathered The digital units (8) of modulation /demodulation module (2) are sent to, digital units (8) are modulated to flight parameter, and DA is converted into intermediate frequency Analogue signal, give remote measurement transmitter unit (6), the upconverting unit (9) of remote measurement transmitter unit (6) is by the analogue signal of intermediate frequency Up-conversion, pre-amplifier unit (10) are fed to power amplifier components (3) after carrying out pre-amplification to up-conversion signal, power amplifier components (3) will Signal delivers to L/S dual-band antennas (1) Microwave emission to ground control centre after amplifying, complete the collection transmission of telemetry;
L/S dual-band antennas (1) receive the peace control signal that ground control centre sends, and are fed to modulation /demodulation module (2), After entering modulation /demodulation module (2), first pass around the device assembly that accepts filter (4) and suppress out-of-band interference and image frequency, then by receiving The low-noise amplifier (11) for sending out peace control receiving unit (7) in component (5) carries out low noise amplification, the signal and mixing after amplification The comprehensive signal of frequency in wave filter (12) carries out being mixed, filter after enter AGC amplifier (13) and be amplified, the intermediate frequency letter after amplification Number be digitized demodulation process by digital units (8), the safety control command after most demodulating at last according to regulation form export to Signal and power supply processing unit, complete the transmission of safety control command.
Beneficial effect:
The peace control remote measurement integrated module of the present invention, it is achieved that reception antenna is integrated with remote measurement transmitting antenna sets for peace control Meter;Highly integrated circuit design is taken, Miniaturization Design is realized;Working frequency range, bit rate can be arranged, communication cycle is adaptive Should, realize General design;Reduce design cost simultaneously, various guided missile, the examination of unmanned plane target, batch inspection, the flight of war instruction can be met Parameter acquisition, record and security control demand.
Description of the drawings
Fig. 1 peace control remote measurement integrated module composition frame charts
Wherein, 1-L/S dual-band antennas 2- modulation /demodulation module 3- power amplifier components 4- accept filter component 5- transmitting-receiving Component 6- remote measurement transmitter units 7- peace control receiving unit 8- digital units 9- upconverting unit 10- pre-amplifier unit 11- Low-noise amplifier 12- mixing filter 13-AGC amplifiers
Specific embodiment
The present invention is described in further detail with reference to embodiment, but embodiments of the present invention not limited to this.
Peace control remote measurement integrated module composition frame chart is as shown in accompanying drawing 1.
Peace control remote measurement integrated module is made up of L/S dual-band antennas 1 and modulation /demodulation module 2.Modulation /demodulation module 2 by Power amplifier components 3, the component 4 that accepts filter, 5 integrated design of transmitting-receiving subassembly composition.Transmitting-receiving subassembly 5 includes peace control receiving unit 7, distant Survey transmitter unit 6, digital units 8.Peace control receiving unit 7 includes low-noise amplifier 11, mixing filter 12, AGC amplifier 13.Remote measurement transmitter unit 6 includes upconverting unit 9, pre-amplifier unit 10.
External signal is powered to peace control remote measurement integrated module with power supply processing unit, while by the guided missile of collection and point being System flight parameter pcm stream is sent to digital units 8, and digital units 8 are modulated to pcm stream, and DA is converted into intermediate frequency and is The analogue signal of 70MHz, gives remote measurement transmitter unit 6, and intermediate frequency is 70MHz's by the upconverting unit 10 of remote measurement transmitter unit 6 Analogue signal up-conversion is fed to power amplifier components 3 to S-band signal, pre-amplifier unit 9 after carrying out pre-amplification to S-band signal, Power amplifier components 3 deliver to 1 Microwave emission of L/S dual-band antennas after S-band letter is amplified.
L/S dual-band antennas 1 receive the peace control signal that ground control centre sends, and are fed to modulation /demodulation module 2.Enter After modulation /demodulation module 2, first pass around the device assembly 4 that accepts filter and suppress out-of-band interference and image frequency, then by transmitting-receiving subassembly 5 The low-noise amplifier 11 of peace control receiving unit 7 carries out low noise amplification, connecing in the signal after amplification and mixing filter 12 Receive the comprehensive signal of frequency carry out being mixed, filter after enter intermediate frequency AGC amplifier 13 and be amplified, the intermediate-freuqncy signal after amplification is by digital single Unit 8 is digitized, demodulation process, and the safety control command after most demodulating at last is exported by RS-422 interfaces according to the form of regulation To external signal and power supply processing unit.

Claims (1)

1. a kind of peace controls remote measurement integration general module, including:L/S dual-band antennas (1) and modulation /demodulation module (2);Wherein, Modulation /demodulation module (2) includes power amplifier components (3), the component that accepts filter (4), transmitting-receiving subassembly (5);Transmitting-receiving subassembly (5) includes distant Survey transmitter unit (6), peace control receiving unit (7), digital units (8);Remote measurement transmitter unit (6) includes upconverting unit (9), pre- Amplifying unit (10);Peace control receiving unit (7) includes low-noise amplifier (11), mixing filter (12), AGC amplifier (13);
Powered to the peace control integrated general module of remote measurement by signal and power supply processing unit, while the flight parameter transmission by collection To the digital units (8) of modulation /demodulation module (2), digital units (8) are modulated to flight parameter, and DA is converted into the mould of intermediate frequency Intend signal, give remote measurement transmitter unit (6), the upconverting unit (9) of remote measurement transmitter unit (6) will become in the analogue signal of intermediate frequency Frequently, pre-amplifier unit (10) is fed to power amplifier components (3) after carrying out pre-amplification to up-conversion signal, and power amplifier components (3) are by signal L/S dual-band antennas (1) Microwave emission is delivered to after amplification to ground control centre, completes the collection transmission of telemetry;
L/S dual-band antennas (1) receive the peace control signal that ground control centre sends, and are fed to modulation /demodulation module (2), enter After modulation /demodulation module (2), first pass around the device assembly that accepts filter (4) and suppress out-of-band interference and image frequency, then pass through transmitting-receiving group In part (5), the low-noise amplifier (11) of peace control receiving unit (7) carries out low noise amplification, the signal and mixing and filtering after amplification The comprehensive signal of frequency in device (12) carries out being mixed, filter after enter AGC amplifier (13) and be amplified, the intermediate-freuqncy signal after amplification by Digital units (8) are digitized demodulation process, and the safety control command after most demodulating at last is exported to signal according to the form of regulation With power supply processing unit, the transmission of safety control command is completed.
CN201611058920.4A 2016-11-24 2016-11-24 A kind of peace control remote measurement integration general module Pending CN106506032A (en)

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Application Number Priority Date Filing Date Title
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CN106506032A true CN106506032A (en) 2017-03-15

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107776912A (en) * 2017-09-15 2018-03-09 江西洪都航空工业集团有限责任公司 A kind of aircraft ground TT&C system net of center control
CN108173604A (en) * 2017-11-23 2018-06-15 北京宇航***工程研究所 Send impulse coding modulation code stream and the device and method of data
CN112071048A (en) * 2020-08-04 2020-12-11 北京临近空间飞行器***工程研究所 Wireless control and telemetry data transmission integrated system
CN114153164A (en) * 2021-11-11 2022-03-08 北京临近空间飞行器***工程研究所 Wireless remote control system for measurement, launch and control

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CN101145825A (en) * 2007-10-30 2008-03-19 航天东方红卫星有限公司 Small satellite satellite-ground communication integrated system
CN102333057A (en) * 2011-05-25 2012-01-25 北京航空航天大学 Micro/nano satellite measure and control communication integral transmitting and receiving system and realization method thereof
CN102355297A (en) * 2011-07-05 2012-02-15 成都睿兴通电子科技有限公司 Receiver array based aviation telemetering system and implementation method thereof
CN103067326A (en) * 2012-12-10 2013-04-24 上海航天测控通信研究所 Telemetering and data transmission integrated transmitter
CN104485974A (en) * 2014-11-26 2015-04-01 成都中远信电子科技有限公司 Radio frequency module for remote metering, remote control and data transmission system of unmanned aerial vehicle and using method of radio frequency module
CN105933054A (en) * 2016-07-07 2016-09-07 上海航天测控通信研究所 Security control device for carrier rocket

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Publication number Priority date Publication date Assignee Title
CN2720730Y (en) * 2004-08-26 2005-08-24 南京才华科技集团有限公司 Integrated radio-frequency receiving-transmitting device
CN101145825A (en) * 2007-10-30 2008-03-19 航天东方红卫星有限公司 Small satellite satellite-ground communication integrated system
CN102333057A (en) * 2011-05-25 2012-01-25 北京航空航天大学 Micro/nano satellite measure and control communication integral transmitting and receiving system and realization method thereof
CN102355297A (en) * 2011-07-05 2012-02-15 成都睿兴通电子科技有限公司 Receiver array based aviation telemetering system and implementation method thereof
CN103067326A (en) * 2012-12-10 2013-04-24 上海航天测控通信研究所 Telemetering and data transmission integrated transmitter
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107776912A (en) * 2017-09-15 2018-03-09 江西洪都航空工业集团有限责任公司 A kind of aircraft ground TT&C system net of center control
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CN108173604A (en) * 2017-11-23 2018-06-15 北京宇航***工程研究所 Send impulse coding modulation code stream and the device and method of data
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CN112071048A (en) * 2020-08-04 2020-12-11 北京临近空间飞行器***工程研究所 Wireless control and telemetry data transmission integrated system
CN114153164A (en) * 2021-11-11 2022-03-08 北京临近空间飞行器***工程研究所 Wireless remote control system for measurement, launch and control

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Application publication date: 20170315