CN108107426A - A kind of radio altimeter - Google Patents
A kind of radio altimeter Download PDFInfo
- Publication number
- CN108107426A CN108107426A CN201810095186.1A CN201810095186A CN108107426A CN 108107426 A CN108107426 A CN 108107426A CN 201810095186 A CN201810095186 A CN 201810095186A CN 108107426 A CN108107426 A CN 108107426A
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- Prior art keywords
- module
- digital signal
- signal processing
- processing module
- programmable logic
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Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/882—Radar or analogous systems specially adapted for specific applications for altimeters
Abstract
The invention discloses a kind of radio altimeters, including microprocessor control system, receiving module, transmitting module, digital signal processing module, it is characterized in that digital signal processing module generates pseudo noise code and two-way clock, the pseudo noise code and all the way clock input to transmitting module, and another way clock inputs to receiving module;Digital signal processing module output processing data, digital signal processing module includes A/D converters, programmable logic device FPGA, high-speed dsp chip and RS422, RS232 data interface chip, the programmable logic device FPGA includes impulse scaler, phase accumulator and wave memorizer, and the impulse scaler, phase accumulator, wave memorizer are sequentially connected.Radio altimeter of the present invention uses FPGA, and advantage is level of integrated system height, few without peripheral auxiliary circuits or requirement, has the characteristics that reliability is high, use scope is extensive, is suitble to promote and apply.
Description
Technical field
The invention belongs to radio application technical fields, specifically, are related to a kind of radio altimeter.
Background technology
Radio altimeter is important fly as survey aircraft to the airborne radio installation of ground vertical range
One of row instruments and meters.The height that it is measured is the true altitude on plane distance ground, is made of transceiver, antenna and indicator.
Using ground (or sea) as a kind of height finding radar of reflecting surface.It can accurate survey aircraft be from the ground in a variety of weather conditions
The relative altitude on (or sea) is one of necessary navigation equipment on modern aircraft.Also known as radar altimeter (Radar
Altimeter).It is different by modulation system, it is divided into CW with frequency modulation radio altimeter and impulse modulation radio altimeter.This
As long as the radio altimeter design of two kinds of systems is reasonable, very high altimetry precision is can reach, is obtained for and is widely applied.
The realization of radio altimeter hardware system needs to use accumulator and D/A converter when using DDS technology composite signals.It is cumulative
Device is generally realized by the controller of system.Simultaneously as the needs of timing control, circuit is also required to controller as control
Center.In the prior art using traditional controller, such as microcontroller.Above-mentioned control function can undoubtedly be realized using microcontroller,
Main problem is the more complicated peripheral circuit of microcontroller needs, such as crystal oscillator and memory etc., this is to system
Reliability brings hidden danger, because complicated circuit is more susceptible to failure, so as to limit its use environment, cannot push away
Wide application.Due to early stage airborne radio altimeter there are circuit level it is low, be not easy to split, measurability is poor the shortcomings of, cause
Its during the test there are measurability it is not high, safeguard and the problems such as maintenance time is long.
The content of the invention
It is an object of the invention to overcome above-mentioned technology there are the defects of, provide a kind of radio altimeter, which adopts
With FPGA, advantage is level of integrated system height, few without peripheral auxiliary circuits or requirement, can carry out self-test, having can
By the characteristics of property is high, use scope is extensive, it is suitble to promote and apply.
Its specific technical solution is:
A kind of radio altimeter, including microprocessor control system, receiving module, transmitting module, digital signal processing module,
Digital signal processing module generates pseudo noise code and two-way clock, all the way pseudo noise code and clock input to transmitting module, separately
Clock inputs to receiving module all the way;Digital signal processing module output processing data, digital signal processing module become including A/D
Parallel operation, programmable logic device FPGA, high-speed dsp chip and RS422, RS232 data interface chip, the programmable logic device
Part FPGA includes impulse scaler, phase accumulator and wave memorizer, the impulse scaler, phase-accumulated
Device, wave memorizer are sequentially connected, and the microprocessor control system is connected with the programmable logic device FPGA, described micro-
Processor control system includes selftest module, infrared distance measurement module and alarm module;The selftest module is automatic for altimeter
Detection;The infrared distance measurement module is for measurement height;The alarm module sends for altimeter when there are abnormal conditions
Alarm.
The content that the selftest module is tested includes altimeter system test, LRU tests, SRU tests, altimeter complete machine
Test includes consuming the indexs such as power, sensitivity, a signal, inspection state, working frequency, output power and altimetry error
Test, LRU tests include sensitivity, a signal, working frequency, output power, altimetry error, voice signal, opposite instruction
Highly dangerous signal provides the test of the indexs such as error, index error, white red illumination, and SRU tests include fault-signal, well
The test of the indexs such as signal, residual altitude, total surplus height, U manipulation signals.
Further, the circuit of the programmable logic device FPGA includes constant-temperature crystal oscillator, selecting switch, general purpose I/O, outside
Memory, linear voltage regulator.
Compared with prior art, beneficial effects of the present invention:
Radio altimeter of the present invention uses FPGA, and advantage is level of integrated system height, without peripheral auxiliary circuits or requirement
Seldom, have the characteristics that reliability is high, use scope is extensive, be suitble to promote and apply.
Description of the drawings
Fig. 1 is the structure diagram of the FPGA of radio altimeter of the present invention;
Fig. 2 is the circuit composition frame chart of the FPGA of radio altimeter of the present invention.
Specific embodiment
Technical scheme is described in more detail in the following with reference to the drawings and specific embodiments.
With reference to Fig. 1-Fig. 2, a kind of radio altimeter, including microprocessor control system, receiving module, transmitting module,
Digital signal processing module, digital signal processing module generate pseudo noise code and two-way clock, all the way pseudo noise code and clock
Transmitting module is inputed to, another way clock inputs to receiving module;Digital signal processing module output processing data, digital signal
Processing module includes A/D converters, programmable logic device FPGA, high-speed dsp chip and RS422, RS232 data-interface core
Piece, the programmable logic device FPGA include impulse scaler, phase accumulator and wave memorizer, the pulse point
Frequency counter, phase accumulator, wave memorizer are sequentially connected, the microprocessor control system and the programmable logic device
Part FPGA connections, the microprocessor control system include selftest module, infrared distance measurement module and alarm module;The self-test mould
Block detects automatically for altimeter;The infrared distance measurement module is for measurement height;The alarm module is going out for altimeter
Alarm is sent during existing abnormal conditions.
The content that the selftest module is tested includes altimeter system test, LRU tests, SRU tests, altimeter complete machine
Test includes consuming the indexs such as power, sensitivity, a signal, inspection state, working frequency, output power and altimetry error
Test, LRU tests include sensitivity, a signal, working frequency, output power, altimetry error, voice signal, opposite instruction
Highly dangerous signal provides the test of the indexs such as error, index error, white red illumination, and SRU tests include fault-signal, well
The test of the indexs such as signal, residual altitude, total surplus height, U manipulation signals.
The foregoing is only a preferred embodiment of the present invention, protection scope of the present invention is without being limited thereto, it is any ripe
Those skilled in the art are known in the technical scope of present disclosure, the letter for the technical solution that can be become apparent to
Altered or equivalence replacement are each fallen in protection scope of the present invention.
Claims (2)
1. a kind of radio altimeter, including microprocessor control system, receiving module, transmitting module, Digital Signal Processing mould
Block, it is characterised in that digital signal processing module generates pseudo noise code and two-way clock, and the pseudo noise code and all the way clock input
To transmitting module, another way clock inputs to receiving module;Digital signal processing module output processing data, Digital Signal Processing
Module includes A/D converters, programmable logic device FPGA, high-speed dsp chip and RS422, RS232 data interface chip,
It is characterized in that, the programmable logic device FPGA includes impulse scaler, phase accumulator and wave memorizer, described
Impulse scaler, phase accumulator, wave memorizer are sequentially connected, the microprocessor control system and described programmable
Logical device FPGA connections, the microprocessor control system include selftest module, infrared distance measurement module and alarm module;It is described
Selftest module detects automatically for altimeter;The infrared distance measurement module is for measurement height;The alarm module is for height
Table sends alarm when there are abnormal conditions.
2. radio altimeter according to claim 1, which is characterized in that the circuit of the programmable logic device FPGA
Including constant-temperature crystal oscillator, selecting switch, general purpose I/O, external memory, linear voltage regulator.
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CN201810095186.1A CN108107426A (en) | 2018-01-31 | 2018-01-31 | A kind of radio altimeter |
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CN201810095186.1A CN108107426A (en) | 2018-01-31 | 2018-01-31 | A kind of radio altimeter |
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CN108107426A true CN108107426A (en) | 2018-06-01 |
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CN201810095186.1A Pending CN108107426A (en) | 2018-01-31 | 2018-01-31 | A kind of radio altimeter |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109959926A (en) * | 2017-12-25 | 2019-07-02 | 大连楼兰科技股份有限公司 | A kind of radar altimeter |
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CN201191184Y (en) * | 2008-03-11 | 2009-02-04 | 陕西长岭电子科技有限责任公司 | Digital wireless electric height meter |
CN201600449U (en) * | 2009-12-30 | 2010-10-06 | 南京誉葆科技有限公司 | Front end device for integrated microwave altimeter |
CN101894219A (en) * | 2010-07-23 | 2010-11-24 | 北京航空航天大学 | Method for quantitative analysis of comprehensive testing coverage of system structure, functions and performance |
CN103941746A (en) * | 2014-03-29 | 2014-07-23 | 国家电网公司 | System and method for processing unmanned aerial vehicle polling image |
CN104238417A (en) * | 2014-09-15 | 2014-12-24 | 西安电子科技大学 | Digital atmosphere data computer and implementation method thereof |
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CN109959926A (en) * | 2017-12-25 | 2019-07-02 | 大连楼兰科技股份有限公司 | A kind of radar altimeter |
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