CN110780267A - Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator - Google Patents

Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator Download PDF

Info

Publication number
CN110780267A
CN110780267A CN201911050615.4A CN201911050615A CN110780267A CN 110780267 A CN110780267 A CN 110780267A CN 201911050615 A CN201911050615 A CN 201911050615A CN 110780267 A CN110780267 A CN 110780267A
Authority
CN
China
Prior art keywords
signal
receiver
transmitter
self
channel
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.)
Granted
Application number
CN201911050615.4A
Other languages
Chinese (zh)
Other versions
CN110780267B (en
Inventor
杜世勇
张尧
程小峡
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sichuan Jiuzhou ATC Technology Co Ltd
Original Assignee
Sichuan Jiuzhou ATC Technology 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 Sichuan Jiuzhou ATC Technology Co Ltd filed Critical Sichuan Jiuzhou ATC Technology Co Ltd
Priority to CN201911050615.4A priority Critical patent/CN110780267B/en
Publication of CN110780267A publication Critical patent/CN110780267A/en
Application granted granted Critical
Publication of CN110780267B publication Critical patent/CN110780267B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/40Means for monitoring or calibrating

Abstract

The invention discloses a self-checking method for a receiving and transmitting channel of an air traffic control inquiry response simulator, which respectively controls the working frequencies of a transmitter and a receiver through a signal processing module, and designs the channel of a radio-frequency signal of the transmitter into two switchable paths, wherein one path can be output to an antenna port through a front-end amplifier, and the other path can be output to a receiver module through a coupler. When self-checking starts, the signal processing module outputs an excitation pulse signal to the transmitter, the transmitter generates a radio frequency signal and outputs the radio frequency signal to the receiver through the circulator, the receiver obtains a baseband signal after frequency mixing demodulation and then transmits the baseband signal to the signal processing module, and the signal processing module judges whether the receiving and transmitting channel works normally according to the received baseband signal. Engineering practice proves that the detection method is accurate and effective, detection efficiency and reliability of self-checking of the navigation management inquiry response simulator are improved, and labor and material cost is saved.

Description

Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator
Technical Field
The invention belongs to the field of data transmission channel testing, and particularly relates to a receiving and transmitting channel self-checking method of an air traffic control inquiry response simulator.
Background
A Secondary radar (SSR) system comprises an interrogator and a responder, wherein the interrogator of the Secondary radar system can transmit 1030MHZ interrogation signals and receive 1090MHZ response signals of an airborne responder to acquire information such as position, height, flight number, identification codes and the like of a target. The secondary radar system is widely applied to the field of traffic control in civil and military aviation.
The navigation management inquiry response simulator is special detection equipment for detecting whether the secondary radar system works normally or not, and can set the working mode of the navigation management inquiry response simulator to be an interrogator mode or a responder mode through mode configuration, so that the responder and the interrogator are respectively detected. Therefore, as a special detection device of the secondary radar system, firstly, it needs to ensure the normal function of the device itself, and when the navigation inquiry response simulator has a fault, the fault information should be reported to the user. The most important of all detection items is the detection of a receiving channel and a transmitting channel. The secondary radar working frequency comprises 1030MHZ and 1090MHZ, a receiver of the interrogator receives the 1090MHZ response signal, and a transmitter transmits 1030MHZ interrogation signals; the receiver of the transponder receives 1030MHZ interrogation radio frequency signals and the transmitter transmits 1090MHZ reply signals. Due to the inconsistency of the operating frequencies of the transceiving channels, the existing navigation management inquiry response simulator cannot finish the detection of the transceiving channels by only depending on the receiver and the transmitter of the simulator no matter the existing navigation management inquiry response simulator works in an inquiry simulation state or a response simulation state, and the detection of the transceiving channels needs to be realized by an additional self-detection oscillation source or external detection equipment.
That is, the existing navigation management inquiry response simulator can be switched to an inquiry simulator and a response simulator by setting, and the receiving and transmitting channels of the existing navigation management inquiry response simulator can not work at the same frequency in the two working modes, so that the receiving and transmitting channels of the existing navigation management inquiry response simulator need to be detected by external detection equipment or need to be additionally provided with an additional self-detection oscillation source, the method usually needs to consume more time, manpower and material resources and even needs to be additionally provided with additional hardware cost, and the detection efficiency of the navigation management inquiry response simulator is reduced.
Disclosure of Invention
The invention aims to: the invention provides a self-checking method of a transceiving channel of an aviation management inquiry response simulator, aiming at the problem that the self-checking of the transceiving channel of the existing aviation management inquiry response simulator is low in detection efficiency mainly through external detection equipment or through adding an additional self-checking oscillation source.
The purpose of the invention is realized by the following technical scheme:
a self-checking method for a transceiving channel of an air traffic control inquiry response simulator is characterized by at least comprising the following steps:
s1: generating a DPSK modulation signal machine receiving and sending channel control step, generating synchronous DPSK pulse modulation signals to be output to a transmitter, recording the number of generated pulses, controlling the transmitter and a receiver to work at the same frequency, and simultaneously controlling a transmitter switching circuit to be switched to a receiver channel;
s2: after receiving a DPSK pulse modulation signal, a transmitter generates a radio frequency signal which is modulated by a frequency source, and the radio frequency signal is output to a receiver channel through a preceding stage amplification circuit, a switching circuit and a coupler;
s3: a receiver frequency mixing, demodulation and demodulated signal output step, wherein after receiving a radio frequency signal, the receiver performs frequency mixing and demodulation on the signal and outputs a demodulated signal;
s4: and a step of detecting, comparing and outputting a detection result of the demodulated signal, namely, finishing the comparison with the recorded pulse quantity based on the received DPSK demodulated signal, judging that a receiving and transmitting channel is normal when the received pulse quantity is consistent with the recorded pulse quantity, judging that the receiving and transmitting channel is abnormal when the received pulse quantity is inconsistent with the recorded pulse quantity, and finishing the output of the judgment result.
According to a preferred embodiment, the step S1 specifically includes the following steps:
s11: a DPSK modulation pulse signal and a transmitter gate control signal are generated by a signal processing module through a counter, the pulse width of the pulse is 0.25us, the number of the pulse is 10, and the pulse width is uniformly distributed in the gate control signal with the length of 6 us;
s12: controlling the transmitter and the receiver to work at the same frequency, and simultaneously controlling the switch circuit of the transmitter to be switched to a channel of the receiver;
s13: the signal processing module records the number of output pulses and detects the number of pulses output by the receiver in real time.
According to a preferred embodiment, in step S12, the transmitter and the receiver are controlled to operate at frequencies 1030MHZ or 1090 MHZ.
According to a preferred embodiment, the DPSK signal in step S2 is generated by: the binary digital baseband signal is differentially encoded and then absolute phase modulated according to the differential code, thereby generating a differential phase shift keying signal.
According to a preferred embodiment, the step S3 specifically includes: s31: after receiving the radio frequency signal, the receiver carries out amplitude limiting, filtering, frequency mixing, demodulation and differential removal on the signal to obtain a DPSK demodulation signal; s32: and outputting the DPSK baseband signal to a signal processing module.
According to a preferred embodiment, said step S4 includes at least:
s41: the signal processing module detects the rising edge of the DPSK pulse signal based on the received DPSK demodulation signal, and stops detecting after the AM gating signal finishes for 2 us;
s42: and comparing the pulse number with the recorded pulse number, judging that the receiving and transmitting channel is normal when the received pulse number is consistent with the recorded pulse number, and judging that the receiving and transmitting channel has a fault when the received pulse number is inconsistent with the recorded pulse number.
According to a preferred embodiment, said step S4 further comprises: s43: and the signal processing module stores the current detection result and transmits the current detection result to a display control interface of the navigation management inquiry response simulator.
The main scheme and the further selection schemes can be freely combined to form a plurality of schemes which are all adopted and claimed by the invention; in the invention, the (non-conflict selections) and other selections can be freely combined. The skilled person in the art can understand that there are many combinations, which are all the technical solutions to be protected by the present invention, according to the prior art and the common general knowledge after understanding the scheme of the present invention, and the technical solutions are not exhaustive herein.
The invention has the beneficial effects that:
1. aiming at the defect that the self-checking function of the conventional navigation management inquiry response simulator is not convenient and quick enough, the invention provides a method for self-checking a receiving and transmitting channel by utilizing a self-body transmitter, a receiver and a signal processing module, so that the time, the labor, the material resources and the hardware cost are saved, the self-checking of the navigation management inquiry response simulator is efficient and quick, and the detection efficiency of the navigation management inquiry response simulator is improved;
2. aiming at the self-checking function of the navigation management inquiry response simulator, a set of strict and complete self-checking signal processing method is provided, and the high reliability of detection is ensured, so that the correctness and the effectiveness of the navigation management inquiry response simulator serving as a special detection device are ensured.
3. The self-checking method of the navigation management inquiry response simulator provided by the invention is based on an automatic detection principle, and has reference significance for the improvement of the self-checking function of the domestic navigation management inquiry response simulator.
Drawings
FIG. 1 is a schematic flow chart illustrating the steps of the self-test method of the present invention;
fig. 2 is a schematic diagram of the constituent structure of the transmitter of the present invention;
FIG. 3 is a schematic diagram of DPSK signal modulation in step 2 according to the present invention;
FIG. 4 is a schematic diagram of the component architecture of the receiver of the present invention;
fig. 5 is a schematic diagram of DPSK signal demodulation performed in step 3 of the method of the present invention.
Detailed Description
The embodiments of the present invention are described below with reference to specific embodiments, and other advantages and effects of the present invention will be readily apparent to those skilled in the art from the disclosure of the present specification. The invention is capable of other and different embodiments and its several details are capable of modifications and variations in various respects, all without departing from the spirit of the invention. It is to be noted that, in the following embodiments, features in the embodiments may be combined with each other without conflict.
It should be noted that, in order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some embodiments of the present invention, but not all embodiments. The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without any inventive step, are within the scope of the present invention.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings or the orientations or positional relationships that the products of the present invention are conventionally placed in use, and are only used for convenience in describing the present invention and simplifying the description, but do not indicate or imply that the devices or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In addition, it should be noted that, in the present invention, if the specific structures, connection relationships, position relationships, power source relationships, and the like are not written in particular, the structures, connection relationships, position relationships, power source relationships, and the like related to the present invention can be known by those skilled in the art without creative work on the basis of the prior art.
Example 1:
referring to fig. 1, a self-checking method for a transceiving channel of an airline management inquiry response simulator is disclosed, and the self-checking method at least comprises the following steps.
Step S1: generating a DPSK modulation signal transceiver channel control step. And generating a synchronous DPSK pulse modulation signal and outputting the signal to a transmitter, recording the number of generated pulses, controlling the transmitter and the receiver to work at the same frequency, and simultaneously controlling a switch circuit of the transmitter to be switched to a channel of the receiver.
Preferably, the step S1 specifically includes the following steps:
s11: a DPSK modulation pulse signal and a transmitter gate control signal are generated by a signal processing module through a counter, the pulse width of the pulse is 0.25us, the number of the pulse is 10, and the pulse width is uniformly distributed in the gate control signal with the length of 6 us;
s12: controlling the transmitter and the receiver to work at the same frequency, and simultaneously controlling the switch circuit of the transmitter to be switched to a channel of the receiver;
s13: the signal processing module records the number of output pulses and detects the number of pulses output by the receiver in real time.
Further, in step S12, the transmitter and the receiver are controlled to operate at the frequency 1030MHZ or 1090 MHZ.
Step S2: and a step of DPSK signal modulation amplification and output. The schematic block diagram of the transmitter is shown in fig. 2. After receiving the DPSK pulse modulation signal, the transmitter generates a radio frequency signal which is subjected to modulation through a frequency source, and the radio frequency signal is output to a receiver channel through a pre-stage amplification circuit, a switching circuit and a coupler.
The working mode of the transmitter is divided into two states of self-checking transmission and normal transmission, and the radio frequency signal is determined to be transmitted to the receiver or output to an antenna port by controlling the switch circuit.
DPSK (differential phase shift keying) is a technique for transferring digital information by using the relative phase change of carriers of adjacent symbols, and is also called relative phase shift keying. Suppose that For the carrier phase difference of the current code element and the previous code element, a digital information sum can be defined
Figure RE-GDA0002323006960000052
The relationship between is
Figure RE-GDA0002323006960000053
The DPSK signal is generated in the following manner: the binary digital baseband signal is differentially encoded, i.e. absolute code of the digital information sequence is converted into differential code, and then absolute phase modulation is performed according to the differential code, so as to generate differential phase shift keying signal.
Preferably, the DPSK signal modulation principle is shown in fig. 3, and the modulation of the absolute code s (t) into the carrier signal F is realized by the principle diagram shown in fig. 3 DPSK(t)。
Step S3: and the receiver mixes frequency, demodulates and outputs the demodulated signal. The schematic block diagram of the receiver is shown in fig. 4. After receiving the radio frequency signal, the receiver performs frequency mixing and demodulation on the signal and outputs a demodulated signal.
Preferably, the step S3 specifically includes: s31: after receiving the radio frequency signal, the receiver carries out amplitude limiting, filtering, frequency mixing, demodulation and differential removal on the signal to obtain a DPSK demodulation signal. S32: and outputting the DPSK baseband signal to a signal processing module.
The demodulation block diagram is shown in fig. 5. The demodulation of DPSK signal adopts differential coherent demodulation method, the demodulation method is to delay the received DPSK signal by one code element interval T BAnd then multiplied by the DPSK signal itself. The multiplier can play a role of phase comparison, the multiplication result reflects the phase difference of the front code element and the rear code element, and the original digital information can be recovered by sampling judgment after low-pass filtering.
Step S4: and detecting, comparing and outputting a detection result by the demodulation signal. And comparing the received DPSK demodulation signals with the recorded pulse number, judging that the transceiving channel is normal when the received pulse number is consistent with the recorded pulse number, judging that the transceiving channel is abnormal when the received pulse number is inconsistent with the recorded pulse number, and finishing outputting a judgment result.
Preferably, the step S4 includes at least:
s41: and the signal processing module detects the rising edge of the DPSK pulse signal based on the received DPSK demodulation signal, and stops detecting after the AM gating signal is ended for 2 us.
S42: and comparing the pulse number with the recorded pulse number, judging that the receiving and transmitting channel is normal when the received pulse number is consistent with the recorded pulse number, and judging that the receiving and transmitting channel has a fault when the received pulse number is inconsistent with the recorded pulse number.
S43: the signal processing module stores the current detection result and transmits the current detection result to a display control interface of the navigation management inquiry response simulator.
The self-checking method for the receiving and transmitting channel of the navigation management inquiry response simulator provided by the invention is characterized in that the working frequencies of a transmitter and a receiver are respectively controlled by a signal processing module, the channel of a radio frequency signal of the transmitter is designed into two switchable paths, one path can be output to an antenna port through a front-end amplifier, and the other path can be output to a receiver module through a coupler. When the self-checking starts, the signal processing module outputs an excitation pulse signal to the transmitter, the transmitter generates a radio frequency signal and outputs the radio frequency signal to the receiver through the circulator, the receiver performs frequency mixing demodulation to obtain a baseband signal and then transmits the baseband signal to the signal processing module, and the signal processing module judges whether the receiving and transmitting channel works normally according to the received baseband signal.
Engineering practice proves that the detection method is accurate and effective, the detection efficiency and reliability of the self-detection of the navigation management inquiry response simulator are improved, and the labor cost and the material cost are saved. Meanwhile, the self-checking method of the receiving and sending module of the navigation management inquiry response simulator provided by the invention has a certain reference function for the improvement of the self-checking function of the domestic navigation management inquiry response simulator.
The foregoing basic embodiments of the invention and their various further alternatives can be freely combined to form multiple embodiments, all of which are contemplated and claimed herein. In the scheme of the invention, each selection example can be combined with any other base example and selection example at will. Numerous combinations will be known to those skilled in the art.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents and improvements made within the spirit and principle of the present invention are intended to be included within the scope of the present invention.

Claims (7)

1. A self-checking method for a transceiving channel of an air traffic control inquiry response simulator is characterized by at least comprising the following steps:
s1: generating a DPSK modulation signal machine receiving and sending channel control step, generating synchronous DPSK pulse modulation signals to be output to a transmitter, recording the number of generated pulses, controlling the transmitter and a receiver to work at the same frequency, and simultaneously controlling a transmitter switch circuit to be switched to a receiver channel;
s2: after receiving the DPSK pulse modulation signal, the transmitter generates a radio frequency signal which is modulated by a frequency source, and the radio frequency signal is output to a receiver channel through a pre-stage amplification circuit, a switching circuit and a coupler;
s3: a receiver frequency mixing, demodulation and demodulated signal output step, wherein after receiving the radio frequency signal, the receiver carries out frequency mixing and demodulation on the signal and outputs a demodulated signal;
s4: and a step of detecting, comparing and outputting a detection result of the demodulated signal, namely comparing the received DPSK demodulated signal with the recorded pulse number, judging that a receiving and transmitting channel is normal when the received pulse number is consistent with the recorded pulse number, judging that the receiving and transmitting channel is abnormal when the received pulse number is inconsistent with the recorded pulse number, and outputting a judgment result.
2. The self-checking method for the transceiving channel of the navigation management inquiry response simulator according to claim 1, wherein the step S1 specifically comprises the following steps:
s11: a DPSK modulation pulse signal and a transmitter gate control signal are generated by a signal processing module through a counter, the pulse width of the pulse is 0.25us, the number of the pulse is 10, and the pulse is uniformly distributed in the gate control signal with the length of 6 us;
s12: controlling the transmitter and the receiver to work at the same frequency, and simultaneously controlling the switch circuit of the transmitter to be switched to a channel of the receiver;
s13: the signal processing module records the number of output pulses and detects the number of pulses output by the receiver in real time.
3. The self-checking method for the transceiving channel of the navigation management inquiry response simulator according to claim 2, wherein in step S12, the transmitter and the receiver are controlled to operate at a frequency of 1030MHZ or 1090 MHZ.
4. The self-checking method for the transceiving channel of the navigation management inquiry response simulator according to claim 1, wherein the DPSK signal in step S2 is generated in a manner that: the binary digital baseband signal is differentially encoded and then absolute phase modulated according to the differential code, thereby generating a differential phase shift keying signal.
5. The self-checking method for the transceiving channel of the navigation management inquiry response simulator according to claim 1, wherein the step S3 specifically comprises:
s31: after receiving the radio frequency signal, the receiver carries out amplitude limiting, filtering, frequency mixing, demodulation and differential removal on the signal to obtain a DPSK demodulation signal;
s32: and outputting the DPSK baseband signal to a signal processing module.
6. The self-checking method for the transceiving channel of the navigation management inquiry response simulator according to claim 1, wherein the step S4 at least comprises:
s41: the signal processing module detects the rising edge of the DPSK pulse signal based on the received DPSK demodulation signal, and stops detecting after the AM gating signal finishes for 2 us;
s42: and comparing the pulse number with the recorded pulse number, judging that the transceiving channel is normal when the received pulse number is consistent with the recorded pulse number, and judging that the transceiving channel has a fault when the received pulse number is inconsistent with the recorded pulse number.
7. The self-checking method for the transceiving channel of the navigation management inquiry response simulator according to claim 6, wherein the step S4 further comprises:
s43: and the signal processing module stores the current detection result and transmits the current detection result to a display control interface of the navigation management inquiry response simulator.
CN201911050615.4A 2019-10-31 2019-10-31 Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator Active CN110780267B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911050615.4A CN110780267B (en) 2019-10-31 2019-10-31 Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911050615.4A CN110780267B (en) 2019-10-31 2019-10-31 Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator

Publications (2)

Publication Number Publication Date
CN110780267A true CN110780267A (en) 2020-02-11
CN110780267B CN110780267B (en) 2021-06-11

Family

ID=69388132

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201911050615.4A Active CN110780267B (en) 2019-10-31 2019-10-31 Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator

Country Status (1)

Country Link
CN (1) CN110780267B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112558025A (en) * 2020-11-30 2021-03-26 四川九洲空管科技有限责任公司 Secondary radar inquiry and response function detection equipment
CN113206697A (en) * 2021-03-19 2021-08-03 中国电子科技集团公司第二十九研究所 Broadband radio frequency receiving and processing system device and self-checking method thereof
CN115085748A (en) * 2022-08-22 2022-09-20 四川九洲空管科技有限责任公司 Method, device and equipment for resisting asynchronous interference

Citations (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2059709A (en) * 1979-09-19 1981-04-23 Marconi Co Ltd Marine transponder system
CN2062853U (en) * 1989-09-07 1990-09-26 交通部天津海上安全监督局 Portable tester for radar responser
US20040205350A1 (en) * 2000-08-28 2004-10-14 Paul Waterhouse Low cost secure ID card and system
WO2008065328A2 (en) * 2006-10-12 2008-06-05 Qinetiq Limited Method and apparatus for determining dme reply efficiency
CN201576743U (en) * 2009-12-14 2010-09-08 深圳市远望谷信息技术股份有限公司 Antenna used in transmission module of CTCS responser
CN101960327A (en) * 2008-02-25 2011-01-26 Iad信息自动化及数据处理有限公司 Carry out the apparatus and method that direction is estimated and decoded by means of the secondary radar signal with improvement
CN102055538A (en) * 2010-11-25 2011-05-11 南京恩瑞特实业有限公司 Self-detection method for unifrequency source of traffic collision avoidance system simulator
CN102183764A (en) * 2010-12-31 2011-09-14 成都天奥信息科技有限公司 Intermediate frequency digital processing method of S-mode interrogation signal
CN202330707U (en) * 2011-11-15 2012-07-11 四川九洲电器集团有限责任公司 Secondary radar response simulator
CN102983919A (en) * 2012-11-14 2013-03-20 中国铁道科学研究院 Detection method of transponder transport module and detection device thereof
CN202949429U (en) * 2012-11-14 2013-05-22 中国铁道科学研究院 Detecting device of transponder transmission module
CN103248439A (en) * 2013-04-08 2013-08-14 贵州航天天马机电科技有限公司 Wireless communication equipment failure detection system and method thereof
CN103399305A (en) * 2013-06-28 2013-11-20 四川九洲空管科技有限责任公司 Amplitude and phase calibration method for radio frequency channels of digital array secondary radar and antenna arrays
CN103684506A (en) * 2013-12-06 2014-03-26 中国航空无线电电子研究所 Radio frequency comprehensive module based on four-unit phased-array antennas multiplexing
CN105070106A (en) * 2015-07-16 2015-11-18 四川九洲空管科技有限责任公司 Airborne collision avoidance system, ACAS transmit-receive host self-detection system and method
CN105070107A (en) * 2015-07-16 2015-11-18 四川九洲空管科技有限责任公司 Airborne collision avoidance system, ACAS transmit-receive host digital signal loop self-detection system and method
CN105281852A (en) * 2015-10-30 2016-01-27 四川九洲电器集团有限责任公司 L-band test equipment and test method
CN106130668A (en) * 2016-08-29 2016-11-16 四川九洲空管科技有限责任公司 A kind of airborne collision avoidance system radio frequency unit self-checking system and self checking method
CN106301413A (en) * 2016-08-16 2017-01-04 中电科现代导航(西安)科技有限公司 The airborne anti-interference reception of ADS B and processing method
CN206038900U (en) * 2016-09-19 2017-03-22 南京恩瑞特实业有限公司 Secondary radar receiver debugging platform
CN108075842A (en) * 2017-12-07 2018-05-25 北京交大思诺科技股份有限公司 A kind of portable BTM detectors
CN109347493A (en) * 2018-11-22 2019-02-15 北京遥感设备研究所 A kind of answering machine simulator depth self-checking circuit
CN109765531A (en) * 2017-11-10 2019-05-17 恩智浦有限公司 Built-in Self Test radar cell and method for phase-shift measurement therein
CN109901150A (en) * 2019-03-04 2019-06-18 四川九洲空管科技有限责任公司 A kind of multifunction array radar device and its detection method

Patent Citations (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2059709A (en) * 1979-09-19 1981-04-23 Marconi Co Ltd Marine transponder system
CN2062853U (en) * 1989-09-07 1990-09-26 交通部天津海上安全监督局 Portable tester for radar responser
US20040205350A1 (en) * 2000-08-28 2004-10-14 Paul Waterhouse Low cost secure ID card and system
WO2008065328A2 (en) * 2006-10-12 2008-06-05 Qinetiq Limited Method and apparatus for determining dme reply efficiency
CN101960327A (en) * 2008-02-25 2011-01-26 Iad信息自动化及数据处理有限公司 Carry out the apparatus and method that direction is estimated and decoded by means of the secondary radar signal with improvement
CN201576743U (en) * 2009-12-14 2010-09-08 深圳市远望谷信息技术股份有限公司 Antenna used in transmission module of CTCS responser
CN102055538A (en) * 2010-11-25 2011-05-11 南京恩瑞特实业有限公司 Self-detection method for unifrequency source of traffic collision avoidance system simulator
CN102183764A (en) * 2010-12-31 2011-09-14 成都天奥信息科技有限公司 Intermediate frequency digital processing method of S-mode interrogation signal
CN202330707U (en) * 2011-11-15 2012-07-11 四川九洲电器集团有限责任公司 Secondary radar response simulator
CN102983919A (en) * 2012-11-14 2013-03-20 中国铁道科学研究院 Detection method of transponder transport module and detection device thereof
CN202949429U (en) * 2012-11-14 2013-05-22 中国铁道科学研究院 Detecting device of transponder transmission module
CN103248439A (en) * 2013-04-08 2013-08-14 贵州航天天马机电科技有限公司 Wireless communication equipment failure detection system and method thereof
CN103399305A (en) * 2013-06-28 2013-11-20 四川九洲空管科技有限责任公司 Amplitude and phase calibration method for radio frequency channels of digital array secondary radar and antenna arrays
CN103684506A (en) * 2013-12-06 2014-03-26 中国航空无线电电子研究所 Radio frequency comprehensive module based on four-unit phased-array antennas multiplexing
CN105070106A (en) * 2015-07-16 2015-11-18 四川九洲空管科技有限责任公司 Airborne collision avoidance system, ACAS transmit-receive host self-detection system and method
CN105070107A (en) * 2015-07-16 2015-11-18 四川九洲空管科技有限责任公司 Airborne collision avoidance system, ACAS transmit-receive host digital signal loop self-detection system and method
CN105281852A (en) * 2015-10-30 2016-01-27 四川九洲电器集团有限责任公司 L-band test equipment and test method
CN106301413A (en) * 2016-08-16 2017-01-04 中电科现代导航(西安)科技有限公司 The airborne anti-interference reception of ADS B and processing method
CN106130668A (en) * 2016-08-29 2016-11-16 四川九洲空管科技有限责任公司 A kind of airborne collision avoidance system radio frequency unit self-checking system and self checking method
CN206038900U (en) * 2016-09-19 2017-03-22 南京恩瑞特实业有限公司 Secondary radar receiver debugging platform
CN109765531A (en) * 2017-11-10 2019-05-17 恩智浦有限公司 Built-in Self Test radar cell and method for phase-shift measurement therein
CN108075842A (en) * 2017-12-07 2018-05-25 北京交大思诺科技股份有限公司 A kind of portable BTM detectors
CN109347493A (en) * 2018-11-22 2019-02-15 北京遥感设备研究所 A kind of answering machine simulator depth self-checking circuit
CN109901150A (en) * 2019-03-04 2019-06-18 四川九洲空管科技有限责任公司 A kind of multifunction array radar device and its detection method

Non-Patent Citations (7)

* Cited by examiner, † Cited by third party
Title
BOAVENTURA A等: "Perfect Isolation: Dealing with Self-Jamming in Passive RFID Systems", 《IEEE MICROWAVE MAGAZINE》 *
BRANDES, S等: "Techniques for ensuring co-existence between B-VHF and legacy VHF systems", 《2006 IEEE AEROSPACE CONFERENCE》 *
PARHI, SS等: "《DESIGN AND FPGA VERIFICATION OF HF RFID TRANSPONDER》", 《 2012 INTERNATIONAL CONFERENCE ON COMMUNICATIONS, DEVICES AND INTELLIGENT SYSTEMS (CODIS)》 *
SUGIANA A 等: "Infrared system for intermittent Automatic train protection", 《2015 15TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS)》 *
宋晓光 等: "中国优秀硕士学位论文全文数据库工程科技Ⅱ辑", 《空间控制技术与应用》 *
张珂: "雷达敌我识别系统研究与应答模拟器设计", 《中国优秀硕士学位论文全文数据库 信息科技辑》 *
罗剑: "无人机载航管应答机外场检查仪的设计与实现", 《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112558025A (en) * 2020-11-30 2021-03-26 四川九洲空管科技有限责任公司 Secondary radar inquiry and response function detection equipment
CN113206697A (en) * 2021-03-19 2021-08-03 中国电子科技集团公司第二十九研究所 Broadband radio frequency receiving and processing system device and self-checking method thereof
CN115085748A (en) * 2022-08-22 2022-09-20 四川九洲空管科技有限责任公司 Method, device and equipment for resisting asynchronous interference

Also Published As

Publication number Publication date
CN110780267B (en) 2021-06-11

Similar Documents

Publication Publication Date Title
CN110780267B (en) Self-checking method for receiving and transmitting channel of navigation management inquiry response simulator
Kumari et al. Investigating the IEEE 802.11 ad standard for millimeter wave automotive radar
CN101517942B (en) Active receiver detection and ranging
US4229737A (en) Ranging system and method for determining the range of a vehicle from a plurality of reference points
CN102549448B (en) Position location using multiple carriers
US20120280862A1 (en) Wireless location detection and/or tracking device and associated methods
AU607667B2 (en) Signal discriminating system
US5859613A (en) System and method for geolocating plural remote transmitters
AU693927B2 (en) Single antenna location and direction finding system
US20040078151A1 (en) Wireless local area network (WLAN) channel radio-frequency identification (RFID) tag system and method therefor
KR100518720B1 (en) DPSK demodulator
WO2012094825A1 (en) Method for locating tag by radio frequency identifying reader and radio frequency identifying reader
US7209040B2 (en) Homodyne RFID receiver and method
CN105450244A (en) Rf receiver with testing capability
WO2003100457A1 (en) Radar transponder
US10917134B2 (en) RFID systems
CN103339524A (en) System for determining the presence of an identifier inside a passenger compartment
US7366465B2 (en) Homodyne RFID receiver and method
CN101401006B (en) Dvor monitor device, and dvor monitor method
CN103353589B (en) Phase-based effective indoor positioning method
CN101159024A (en) Semiconductor integrated circuit device and receiving device
US7734270B2 (en) Method and apparatus for an enhanced RFID tag interrogator
JPH0836052A (en) Intarrogator system to moving body responder
CN108882170B (en) Electronic license plate read-write device
US20220413093A1 (en) Multi-input multi-output radar and mobile tool

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant