CN103323825B - Fault softening method of secondary radar system - Google Patents
Fault softening method of secondary radar system Download PDFInfo
- Publication number
- CN103323825B CN103323825B CN201310299126.9A CN201310299126A CN103323825B CN 103323825 B CN103323825 B CN 103323825B CN 201310299126 A CN201310299126 A CN 201310299126A CN 103323825 B CN103323825 B CN 103323825B
- Authority
- CN
- China
- Prior art keywords
- channel
- state
- weights
- launches
- passage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Abstract
The invention relate to a fault softening method of a secondary radar system. The system comprises two radar channels which are mutually duplicated hot-redundancy, have the same configuration and can independently finish signal receiving and transmitting; and each channel comprises corresponding state site information and gives an appointed weight. The setting requirements of the weight are that an integral multiple relation does not exist between all state weights; a plurality of the state weights are accumulated to be not equal to a certain state weight; and the maximum value of the single state weight is 101 and the minimum value of the single state weight is 10. A data processing module is used for carrying out timing sampling on the state of each LRU (Least Recently Used) module of the channel; a fault total weight of the channel is calculated in real time according to the definition of the weights; a fault total weight of the channel at the opposite side is obtained through communication between the two channels; meanwhile, the fault total weight of the channel is announced to the channel at the opposite side; and when the channel A and the channel B are switched, the channel with the weight which is zero or smaller is switched to be used as a working channel, and the channel with the greater weight is used as a backup channel.
Description
Technical field
The present invention relates to a kind of method evading or reduce fault effects by system oneself adjustment, particularly relate to a kind of method that secondary radar system failure is softening.
Background technology
Along with the development of aviation services, on the one hand to the reliability of aviation management equipment, security, ageingly propose more and more higher requirement; On the other hand, aviation management equipment realizes high automation, unmanned also becomes inexorable trend.Secondary radar is as the major equipment of air traffic control and Routing monitoring; there is very high mission reliability requirement; except the periodic maintenance of equipment, secondary radar needs 24 continuous throughout the twenty-four hour24s, does not shut down and export in real time the target information of continous-stable in radar power coverage all the year round.
Summary of the invention
For above demand, the invention provides one to intervene without the need to equipment use personnel, automatically to finish the work the selection of passage and switching according to equipment state, the not interrupt targets information that reaches exports or reduces the secondary radar system failure softening method that target information exports break period.
The secondary radar that the present invention relates to adopts channel hot standby part working system, 2 radar passages are called A channel and channel B, when a passage is in main channel duty, another passage is in warm standby state, and A, channel B all can serve as the role of main channel or alternate channel.The functional modules such as main channel is launched through inquiry, response reception, signal transacting, data processing complete the work of targeted surveillance and information extraction, and send aviation management center by the target information of acquisition, realize the function of airport monitoring and en route control, index test and status monitoring are carried out to each functional module of main channel simultaneously; Alternate channel does not launch interrogating signal, does not also receive answer signal, but carries out index test and status monitoring to each functional module of this passage in real time.
(forbid automatically switching) under manual work mode, radar operation personnel can check the equipment state of main channel and alternate channel at any time by aobvious control terminal, the craft carrying out main channel and alternate channel at any time between the two channels switches.
When secondary radar two passages are all normal, any one channel setting is in main channel duty, can export correct, continuous print target information.
When secondary radar passage breaks down, when there being operating personnel on duty, main channel can be switched to normal channel, ensure that radar normally can export target information; When two passages of secondary radar have fault, when there being operating personnel on duty, rule of thumb main channel can be switched to the lighter passage of one of them fault, ensure radar not interrupt targets information output, or index use is fallen, still target information can be exported, but aimed quality declines to some extent.
In unattended situation, when secondary radar passage breaks down, and be service aisle when breaking down, radar can interrupt targets information export.
In order to solve the problem, the invention provides a kind of secondary radar system failure softening method, it is characterized in that:
I. its secondary radar system comprises the radar passage of 1 pair of antenna, 1 change-over switch and 2 two-node cluster hot backup each other;
2 described radar passages are called A channel and channel B, and A, channel B all can serve as the role of main channel or alternate channel; Each radar passage is a complete signal receiving and transmitting system, can the signal transmitting and receiving function of complete independently secondary radar;
The hardware configuration of A channel and channel B is just the same, and one of them passage comprises 2 transmitters, 1 receiver, 1 feeder line combination, 1 signal transacting, 1 data processing and 1 integrated drive generator totally 7 LRU modules;
2 corresponding 2 launching beams of transmitter, complete inquiry wave beam Σ respectively, control the transmitting of wave beam Ω;
Feeder line has combined inquiry wave beam Σ, has controlled wave beam Ω transmitting-receiving translation function;
Receiver comprises 3 receiving cables, completes inquiry wave beam Σ respectively, controls the reception of wave beam Ω, difference beam Δ, provide the pumping signal needed for 2 transmitters and the self-test signal needed for receiver self-inspection simultaneously;
Signal processing module completes and carries out video pre-filtering, reply process, code assembling process to receiver input signal, data processing is issued in final generation reply process report, signal processing module, also according to the mode control word that data processing is sent, produces timing and the control signal of whole secondary radar;
Data processing module carries out initial reply process, target location calculatings, broad pulse identification, reply process by the reply process report produced signal processing module, completes the Plot coherence of target, flight path to rise batch and flight path maintenance; The mode of operation that data processing also completes secondary radar system arranges and corresponding mode control word is sent signal transacting, realizes state acquisition and the fault diagnosis of system simultaneously;
Integrated drive generator provides required direct supply for whole secondary radar system;
A channel is connected with antenna by change-over switch with channel B;
By change-over switch, service aisle arbitrarily can switch between A channel and channel B, does not affect echo signal and export during switching; There is information sharing between A channel and channel B and write to each other.
II .A passage arranges identical with the mode bit of channel B, and the mode bit that one of them passage comprises is defined as follows:
Transmitter state information: Σ emitting module is overheated, Ω emitting module is overheated, Σ launches sequential, Ω launches sequential, Σ emissive power; Ω emissive power;
Receiver state information: Σ receiving cable, Δ receiving cable, Ω receiving cable, Σ pumping signal, Ω pumping signal, receiver are combined frequently, self-test signal source;
Feeder line assembled state information: Σ launches forward-wave, Ω launches forward-wave, Σ launches retonation wave, Ω launches retonation wave, Σ launches standing wave, Ω launches standing wave;
Signal transacting status information: PSV state, sign bit state, confidence bit state, Σ if sampling, Δ if sampling, Ω if sampling;
Data processing state information: reply process interrupts, CAN node receives number, bearing signal state, adjacent machine crash;
Integrated drive generator status information :+5V3A power supply status ,+12V3A power supply status ,-12V2A power supply status ,-12V0.5A power supply status ,+24V3A power supply status ,+50V6A power supply status.
The weights definition mode of each mode bit of III .LRU module is as follows:
Each LRU module has multiple mode bit to reflect its different qualities or state, according to the influence degree of each mode bit to this LRU module and entire system performance, give the weights of specifying, larger on the weights of the larger mode bit definition of system performance impact, weights corresponding to same fault are identical;
Not integral multiple relation between the weights that the setting of weights will accomplish each state;
The weights of multiple state add up and are not equal to the weights of certain state, and the maximal value of single status weights is 101, and minimum value is 10.
The pattern that IV .A passage, channel B are run according to weights definition is as follows:
Carry out accumulation by data processing module to the trouble power of this passage to calculate, the trouble power accumulating value of A channel or channel B is larger, illustrate that the fault of this passage is more serious, when automatically switching between A channel and channel B, automatic selection be switched to weights be the passage of zero or less as service aisle, the passage that weights are larger is backup path.
V. softly fail process is as follows:
1) state of data processing module to each LRU module of this passage carries out timing sampling;
2) define according to above-listed weights, calculate the fault total weight value of this passage in real time;
3) by the communication between binary channels, obtain the fault total weight value to square channel, the fault total weight value of this passage is informed square channel simultaneously;
4) arrange according to radar duty, determine whether switch between A channel, channel B.
The weights of each mode bit of described III .LRU module are defined as:
Transmitter: Σ emitting module is overheated=and 20, Ω emitting module is overheated=20, Σ launches sequential=101, Ω launches sequential=81, Σ emissive power=50, Ω emissive power=30;
Receiver: Σ receiving cable=101, Δ receiving cable=80, Ω receiving cable=31, receiver frequently combine=101, self-test signal source=31, Σ pumping signal=51, Ω pumping signal=40;
Feeder line combines: Σ launches forward-wave=101, Ω launches forward-wave=61, Σ launches retonation wave=81, Ω launches retonation wave=41, Σ launches standing wave=60, Ω launches standing wave=40;
Signal transacting: PSV state=101, sign bit state=31, confidence bit state=31, Σ if sampling=60, Δ if sampling weights=40, Ω if sampling=40;
Data processing: number=50, bearing signal state=80, adjacent machine deadlock=30 are received in reply process interruption 101, CAN node;
Integrated drive generator :+5V3A power supply status=61 ,+12V3A power supply status=101 ,-12V2A power supply status=101 ,-12V0.5A power supply status=10 ,+24V3A power supply status 101 ,+50V6A power supply status=101.
Beneficial effect: the secondary radar configuration that the present invention is directed to channel hot standby part, achieves the seamless switching between binary channels.And when certain LRU of single channel breaks down or all have LRU to break down in binary channels, intervene without the need to operating personnel, radar is according to the criterion designed, trouble power is calculated, automatically selection and the switching of service aisle is carried out according to result of calculation, select non-fault or the lighter passage of fault as service aisle, realize evading or being down to minimum by the impact of fault of fault.The not interrupt targets information that reaches exports or reduces the object that target information exports break period.The present invention is applicable to the similar devices of high reliability, binary channels Hot Spare each other.
Accompanying drawing explanation
Fig. 1: the hardware composition frame chart of secondary radar in this patent;
Fig. 2: the detailed status table of the single passage of secondary radar in this patent;
Fig. 3: secondary radar state weights definition in this patent.
Embodiment
Below in conjunction with accompanying drawing, the present invention is described in further detail.
As shown in Figure 1, a kind of secondary radar system failure softening method of the present invention:
I. its secondary radar system comprises the radar passage of 1 pair of antenna, 1 change-over switch and 2 two-node cluster hot backup each other;
2 described radar passages are called A channel and channel B, and be 2 radar passages of Hot Spare each other, A, channel B all can serve as the role of main channel or alternate channel; Each radar passage is a complete signal receiving and transmitting system, can the signal transmitting and receiving function of complete independently secondary radar;
The hardware configuration of A channel and channel B is just the same, and one of them passage comprises 2 transmitters, 1 receiver, 1 feeder line combination, 1 signal transacting, 1 data processing and 1 integrated drive generator totally 7 LRU modules, and LRU is linear replaceable units;
2 corresponding 2 launching beams of transmitter, complete inquiry wave beam Σ respectively, control the transmitting of wave beam Ω;
Feeder line has combined inquiry wave beam Σ, has controlled the conversion of wave beam Ω transmission-receiving function;
Receiver comprises 3 receiving cables, completes inquiry wave beam Σ respectively, controls the reception of wave beam Ω, difference beam Δ, provide the pumping signal needed for transmitter and the self-test signal needed for receiver self-inspection simultaneously;
Signal processing module completes and carries out video pre-filtering, reply process, code assembling process etc. to receiver input signal, data processing is issued in final generation reply process report, signal processing module, also according to the mode control word that data processing is sent, produces timing and the control signal of whole secondary radar;
Data processing module carries out a series of process such as initial reply process, target location calculatings, broad pulse identification, response are relevant by the reply process report produced signal processing module, completes the Plot coherence of target, flight path to rise batch and flight path maintenance; The mode of operation that data processing also completes secondary radar system arranges and corresponding mode control word is sent signal transacting, realizes state acquisition and the fault diagnosis of system simultaneously;
Integrated drive generator provides required direct supply for whole secondary radar system;
A channel is connected with antenna by change-over switch with channel B;
By change-over switch, service aisle arbitrarily can switch between A channel and channel B, does not affect echo signal and export during switching; For ensureing not affect the continuity exporting echo signal when passage bridge, there is information sharing between 2 passages and writing to each other, thus realizing the seamless switching exporting target information.
II .A passage arranges identical with the mode bit of channel B, and Fig. 2 is the single pass status summary table of secondary radar, wherein further comprises online index test value.
The mode bit that each LRU module comprises is defined as follows:
Transmitter state information: Σ emitting module is overheated, Ω emitting module is overheated, Σ launches sequential, Ω launches sequential, Σ launches probability; Ω emissive power;
Receiver state information: Σ receiving cable, Δ receiving cable, Ω receiving cable, Σ pumping signal, Ω pumping signal, receiver are combined frequently, self-test signal source;
Feeder line assembled state information: Σ launches forward-wave, Ω launches forward-wave, Σ launches retonation wave, Ω launches retonation wave, Σ launches standing wave, Ω launches standing wave;
Signal transacting status information: PSV state, sign bit state, confidence bit state, Σ if sampling, Δ if sampling, Ω if sampling;
Data processing state information: reply process interrupts, CAN node receives number, bearing signal state, adjacent machine crash;
Integrated drive generator status information :+5V3A power supply status ,+12V3A power supply status ,-12V2A power supply status ,-12V0.5A power supply status ,+24V3A power supply status ,+50V6A power supply status;
The weights definition mode of each mode bit of III .LRU module is as follows:
Each LRU module has multiple mode bit to reflect its different qualities or state, according to the influence degree of each mode bit to this LRU module and entire system performance, give the weights of specifying, larger on the weights of the larger mode bit definition of system performance impact, weights corresponding to same fault are identical;
Consider the result difference to some extent that multiple state weights are cumulative simultaneously, be convenient to compare, be not integral multiple relation between the weights that the setting of weights will accomplish each state, the weights of multiple state add up and are not equal to the weights of certain state, the maximum weight value of single status is 101, and minimum value is 10.
The pattern that IV .A passage, channel B are run according to weights definition is as follows:
State and the fault collection of secondary radar system modules is completed by data processing, and accumulation calculating is carried out to the trouble power of this passage, the trouble power accumulating value of A channel or channel B is larger, illustrate that the fault of this passage is more serious, when automatically switching between A channel and channel B, automatic selection be switched to weights be the passage of zero or less as service aisle, the passage that weights are larger is backup path;
The weights of each mode bit of LRU define as shown in Figure 3:
Transmitter: Σ emitting module is overheated=and 30, Ω emitting module is overheated=20, Σ launches sequential=101, Ω launches sequential=81, Σ emissive power=51, Ω emissive power=31;
Receiver: Σ receiving cable=101, Δ receiving cable=80, Ω receiving cable=31, Σ pumping signal=51, Ω pumping signal=40, receiver frequently combine=101, self-test signal source=31;
Feeder line combines: Σ launches forward-wave=101, Ω launches forward-wave=61, Σ launches retonation wave=81, Ω launches retonation wave=41, Σ launches standing wave=60, Ω launches standing wave=40;
Signal transacting: PSV state=101, sign bit state=31, confidence bit state=31, Σ if sampling=60, Δ if sampling=40, Ω if sampling=40;
Data processing: number=50, bearing signal state=80, adjacent machine deadlock=30 are received in reply process interruption=101, CAN node;
Integrated drive generator :+5V3A power supply status=61 ,+12V3A power supply status=101 ,-12V2A power supply status=101 ,-12V0.5A power supply status=10 ,+24V3A power supply status 101 ,+50V6A power supply status=101.
Due to the working power that+5V25A power supply is data processing, this power fail can cause that data processing does not work, secondary radar systemic breakdown, cannot carry out state acquisition, fault diagnosis and weight computing, thus do not have in weights definition+5V25A power supply this.
V. the secondary radar softly fail procedure realized based on said system composition and weights definition is as follows:
1) state of data processing module to each LRU module of this passage carries out timing sampling;
2) define according to above-listed weights, calculate the fault total weight value of this passage in real time;
3) by the communication between binary channels, obtain the fault total weight value to square channel, the fault total weight value of this passage is informed square channel simultaneously;
4) arrange according to radar duty, determine whether switch between A channel, channel B.
Due to the difference of radar duty, the 4th) step comprises 2 kinds of situations: 1. allow to automatically switch; 2. forbid automatically switching (manual switchover).Radar can be set to allow automatically switch or forbid to automatically switch (manual switchover) according to the integrity of radar equipment, stability status by user.
Usually when equipment without any fault, stable, radar is set to allow automatically switch.Once there be fault to occur, radar can automatically switch according to real-time fault collection and trouble power result of calculation, and the reliability of such equipment is high and failure rate is minimum.
But in extreme circumstances, there is fault in 1 passage always, or A channel, channel B both have fault to occur, maintenance personal cannot be on the scene at once again and repair, at this moment best selection is set to by radar forbid automatically switching, user rule of thumb manually carries out passage bridge, makes radar be operated in normal channel or the lighter passage of fault.
Here is exactly realize the softening instantiation of the secondary radar system failure, and precondition the mode of operation of radar is set to " allowing to automatically switch ".
Example 1: when A channel does not have fault, A channel fault total weight value is zero;
During " Σ emissive power " fault of channel B, channel B fault total weight value is 51;
Accordingly, secondary radar will automatically switch to the A channel of normal work, and radar normally can export target information.
Example 2: when " Σ emissive power " fault of A channel, A channel fault total weight value is 51;
During " Ω emissive power " fault of channel B, channel B fault total weight value is 31;
Accordingly, secondary radar will automatically switch to the lighter channel B of fault, and radar falls index and uses, and can export target information, but due to channel B " Ω emissive power " fault, radar does not have Sidelobe Suppression function, can cause false alarm rate that normal condition is higher;
Example 3: when " Σ receiving cable " fault of A channel, A channel fault total weight value is 101;
" Δ receiving cable " fault of channel B, channel B fault total weight value is 80;
Accordingly, secondary radar will automatically switch to the lighter channel B of fault, and radar falls index and uses, and can export target information, but due to " Δ receiving cable " fault of channel B, radar does not have monopulse characteristic, and aimed at precision declines to some extent;
Example 4: when " Σ launches forward-wave " fault and " Σ emissive power " fault of A channel, A channel fault total weight value is 152;
" self-test signal source " fault of channel B, channel B fault total weight value is 31;
Accordingly, secondary radar, by automatically switching to the lighter channel B of fault, can export target information, but due to " self-test signal source " fault of channel B, channel B loses receiver self-checking function;
Explanation of nouns:
PSV(Processed Sum Video)---processed and video;
Σ (Σ wave beam, Σ passage)---secondary radar with wave beam or and passage, also claim inquiry wave beam or inquiry passage;
Ω (Ω wave beam, Ω passage)---the control wave beam of secondary radar or control channel, also claims Sidelobe Suppression wave beam or Sidelobe Suppression passage;
The difference beam of Δ (Δ wave beam, Δ passage)---secondary radar or difference passage;
LRU(Line Replaceable Unit)---linear replaceable units;
Forward-wave---incident wave;
Retonation wave---reflection wave;
The ratio of standing wave---incident wave and reflection wave;
Seamless switching---during from a passage bridge to another passage, radar system not interrupt targets exports.
The foregoing is only the preferred embodiments of the present invention, be not restricted to the present invention, for a person skilled in the art, the present invention can have various modifications and variations.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within right of the present invention.
Claims (2)
1. a secondary radar system failure softening method, is characterized in that:
I. its secondary radar system comprises the radar passage of 1 pair of antenna, 1 change-over switch and 2 two-node cluster hot backup each other;
2 described radar passages are called A channel and channel B, and A, channel B can both serve as the role of main channel or alternate channel; Each radar passage is a complete signal receiving and transmitting system, can the signal transmitting and receiving function of complete independently secondary radar;
The hardware configuration of A channel and channel B is just the same, one of them passage comprises 2 transmitters, 1 receiver, 1 feeder line combination, 1 signal processing module, 1 data processing module and 1 integrated drive generator totally 7 LRU modules, and LRU is linear replaceable units;
2 corresponding 2 launching beams of transmitter, complete inquiry wave beam Σ respectively, control the transmitting of wave beam Ω;
Feeder line has combined inquiry wave beam Σ, has controlled the conversion of wave beam Ω transmission-receiving function;
Receiver comprises 3 receiving cables, completes inquiry wave beam Σ respectively, controls the reception of wave beam Ω, difference beam Δ, provide the pumping signal needed for 2 transmitters and the self-test signal needed for receiver self-inspection simultaneously;
Signal processing module completes and carries out video pre-filtering, reply process, code assembling process to receiver input signal, data processing module is issued in final generation reply process report, signal processing module, also according to the mode control word that data processing module is sent, produces timing and the control signal of whole secondary radar;
Data processing module carries out initial reply process, target location calculatings, broad pulse identification, reply process by the reply process report produced signal processing module, completes the Plot coherence of target, flight path to rise batch and flight path maintenance; The mode of operation that data processing module also completes secondary radar system arranges and corresponding mode control word is sent signal processing module, realizes state acquisition and the fault diagnosis of system simultaneously;
Integrated drive generator provides required direct supply for whole secondary radar system;
A channel is connected with antenna by change-over switch with channel B;
By change-over switch, service aisle arbitrarily can switch between A channel and channel B, does not affect echo signal and export during switching; There is information sharing between A channel and channel B and write to each other;
II .A passage arranges identical with the mode bit of channel B, and the mode bit that one of them passage comprises is defined as follows:
Transmitter state information: Σ emitting module is overheated, Ω emitting module is overheated, Σ launches sequential, Ω launches sequential, Σ emissive power; Ω emissive power;
Receiver state information: Σ receiving cable, Δ receiving cable, Ω receiving cable, Σ pumping signal, Ω pumping signal, receiver are combined frequently, self-test signal source;
Feeder line assembled state information: Σ launches forward-wave, Ω launches forward-wave, Σ launches retonation wave, Ω launches retonation wave, Σ launches standing wave, Ω launches standing wave;
Signal processing module status information: PSV state, sign bit state, confidence bit state, Σ if sampling, Δ if sampling, Ω if sampling;
Data processing module status information: reply process interruption, CAN nodes, bearing signal state, adjacent machine are crashed;
Integrated drive generator status information :+5V3A power supply status ,+12V3A power supply status ,-12V2A power supply status ,-12V0.5A power supply status ,+24V3A power supply status ,+50V6A power supply status;
The weights definition mode of each mode bit of III .LRU module is as follows:
Each LRU module has multiple mode bit to reflect its different qualities or state, according to the influence degree of each mode bit to this LRU module and entire system performance, give the weights of specifying, larger on the weights of the larger mode bit definition of system performance impact, weights corresponding to same fault are identical;
Consider the result difference to some extent that multiple state weights are cumulative simultaneously, for ease of comparing, be not integral multiple relation between the weights that the setting of weights will accomplish each state, the weights of multiple state add up and are not equal to the weights of certain state, the maximum weight value of single status is 101, and minimum value is 10;
The pattern that IV .A passage, channel B are run according to weights definition is as follows:
Carry out accumulation by data processing module to the trouble power of this passage to calculate, the trouble power accumulating value of A channel or channel B is larger, illustrate that the fault of this passage is more serious, when automatically switching between A channel and channel B, automatic selection be switched to weights be the passage of zero or less as service aisle, the passage that weights are larger is backup path;
V. softly fail process is as follows:
The state of data processing module to each LRU module of this passage carries out timing sampling;
Define according to above-listed weights, calculate the fault total weight value of this passage in real time;
By the communication between binary channels, obtain the fault total weight value to square channel, simultaneously by the fault of this passage
Total weight value is informed square channel;
Arrange according to radar duty, determine whether switch between A channel, channel B.
2. secondary radar system failure softening method according to claim 1, is characterized in that: the weights of each mode bit of described III .LRU module are defined as:
Transmitter: Σ emitting module is overheated=and 20, Ω emitting module is overheated=20, Σ launches sequential=101, Ω launches sequential=81, Σ emissive power=51, Ω emissive power=31;
Receiver: Σ receiving cable=101, Δ receiving cable=80, Ω receiving cable=31, Σ pumping signal=51, Ω pumping signal=40, receiver frequently combine=101, self-test signal source=31;
Feeder line combines: Σ launches forward-wave=101, Ω launches forward-wave=61, Σ launches retonation wave=81, Ω launches retonation wave=41, Σ launches standing wave=60, Ω launches standing wave=40;
Signal processing module: PSV state=101, sign bit state=31, confidence bit state=31, Σ if sampling=60, Ω if sampling=40, Δ if sampling=40;
Data processing module: reply process interruption=101, bearing signal state=80, CAN nodes=50, adjacent machine crash=30;
Integrated drive generator :+5V3A power supply status=61 ,+12V3A power supply status=101 ,-12V2A power supply status=101 ,-12V0.5A power supply status=10 ,+24V3A power supply status=101 ,+50V6A power supply status=101.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310299126.9A CN103323825B (en) | 2013-07-16 | 2013-07-16 | Fault softening method of secondary radar system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310299126.9A CN103323825B (en) | 2013-07-16 | 2013-07-16 | Fault softening method of secondary radar system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103323825A CN103323825A (en) | 2013-09-25 |
| CN103323825B true CN103323825B (en) | 2014-12-24 |
Family
ID=49192681
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310299126.9A Active CN103323825B (en) | 2013-07-16 | 2013-07-16 | Fault softening method of secondary radar system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103323825B (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105812103B (en) * | 2014-12-30 | 2019-07-19 | 海能达通信股份有限公司 | The method, apparatus and communication system of intermediate station warm back-up |
| CN104954043A (en) * | 2015-06-29 | 2015-09-30 | 中国电子科技集团公司第三十八研究所 | S-band megawatt dual-unit hot standby transmitter and control method thereof |
| CN105099777B (en) * | 2015-07-23 | 2018-09-11 | 南京国电南自轨道交通工程有限公司 | The method of communication gate dual-computer redundancy suitable for track traffic electric power monitoring system |
| CN106597397B (en) * | 2016-12-20 | 2019-03-01 | 中国科学院电子学研究所 | A kind of real time sar imaging processor fault method for rapidly positioning |
| CN108196233B (en) * | 2017-12-26 | 2020-08-25 | 北京无线电测量研究所 | Real-time online calibration method based on millimeter wave cloud detection radar |
| CN111044978A (en) * | 2019-12-10 | 2020-04-21 | 中船航海科技有限责任公司 | Double-transmitter shore-based radar and working method thereof |
| CN113608171B (en) * | 2021-06-21 | 2024-03-19 | 北京无线电测量研究所 | Channel hot backup switching method of push-stage assembly |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102008059424B4 (en) * | 2008-11-27 | 2023-01-19 | IAD Gesellschaft für Informatik, Automatisierung und Datenverarbeitung mbH | Secondary radar system with dynamic sectorization of the space to be monitored using multi-antenna arrangements and methods for this |
| CN202110281U (en) * | 2011-05-31 | 2012-01-11 | 安徽四创电子股份有限公司 | Automatic recombination structure of hollow pipe primary radar apparatus |
| CN202351423U (en) * | 2011-12-12 | 2012-07-25 | 南京恩瑞特实业有限公司 | Air traffic control secondary radar equipment main machine layout structure |
-
2013
- 2013-07-16 CN CN201310299126.9A patent/CN103323825B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN103323825A (en) | 2013-09-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103323825B (en) | Fault softening method of secondary radar system | |
| CN110361979B (en) | Safety computer platform in railway signal field | |
| CN101788817B (en) | Fault recognition and processing method based on satellite-bone bus | |
| CN110351174B (en) | Module redundancy safety computer platform | |
| CN102915038A (en) | Dual-redundancy autonomous flight control system for micro-miniature unmanned helicopters | |
| CN102801767A (en) | Prognostics and health management (PHM) system for single-level aircraft structure and implementation method | |
| CN105891846A (en) | High-reliability base reinforcing system ground station equipment and online switching method | |
| CN109188468A (en) | A kind of ground monitoring system monitoring satellite health | |
| CN102474095A (en) | Substation automation system with remote redundant protection function | |
| GB2459521A (en) | Multilateration system for aircraft location | |
| CN107677996B (en) | On-line detection method for working state of radar system | |
| CN100382040C (en) | Redundant method for micro aircraft GNC system | |
| CA3046477C (en) | Methods and systems for controlling operation of satellite data units of an aircraft | |
| CN105866809A (en) | Ground-based augmentation system ground station equipment with assemblies having hot standby switching function and hot standby switching method | |
| CN106980259B (en) | A kind of dual redundant implementation method of radar transmitter monitoring system | |
| RU2635825C1 (en) | Method of generating self-organizing structure of navigation complex | |
| Gao et al. | Research on architecture of condition monitoring and health management of active electronically scanned array radar | |
| CN100525141C (en) | Method and device for layered priority control of high and low space remote sensing positioning servo of satellite communication | |
| CN113973025A (en) | CAN bus-based satellite-borne computer communication reliability and fault tolerance design method | |
| CN207664982U (en) | A kind of space shuttle communication system based on stabilized power source | |
| Koga et al. | Autonomous decentralized surveillance system and continuous target tracking technology for air traffic control applications | |
| KR102470750B1 (en) | Method for duplexing drone control networks and the control apparatus thereof | |
| EP0524327B1 (en) | Method for Monitoring and Controlling a Transmitting Station for a Position Locating System, particularly for the Microwave Landing System, and Transmitting Station for carrying out such method | |
| US20220155463A1 (en) | Systems and methods for synchronizing satellite-based clock devices | |
| Koga et al. | Autonomous decentralized high-assurance surveillance system for air traffic control |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |