CN105676102A - Method and device for acquiring sensitive section of neutron single event effect device based on FOM - Google Patents

Method and device for acquiring sensitive section of neutron single event effect device based on FOM Download PDF

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CN105676102A
CN105676102A CN201410676788.8A CN201410676788A CN105676102A CN 105676102 A CN105676102 A CN 105676102A CN 201410676788 A CN201410676788 A CN 201410676788A CN 105676102 A CN105676102 A CN 105676102A
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observation
sensitive apparatus
section
cofactor
fom
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CN105676102B (en
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王群勇
陈冬梅
阳辉
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BEIJING SAN-TALKING TESTING ENGINEERING ACADEMY Co Ltd
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BEIJING SAN-TALKING TESTING ENGINEERING ACADEMY Co Ltd
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Abstract

The invention provides a method and a device for acquiring the sensitive section of a neutron single event effect device based on FOM. The method comprises the following steps: using a predetermined radiation source to conduct a ground simulation experiment, acquiring an observation value Sigma(observation) of the sensitive section of the sensitive device, and monitoring the number N(end) of single event effect errors of the sensitive device in the experiment; performing a division operation on a value Sigma(FOM) of the sensitive section of the sensitive device calculated by an FOM method and the observation value Sigma(observation) of the sensitive section of the sensitive device to get a first auxiliary factor; performing a division operation on a value Sigma(Rosetta) of the sensitive section of the sensitive device obtained through Rosetta real environment test and the observation value Sigma(observation) of the sensitive section of the sensitive device to get a second auxiliary factor; calculating the value of a correction factor according to the first auxiliary factor, the second auxiliary factor and the number of single event effect errors; and using the correction factor to correct an observation value Sigma(preset) of the sensitive section of the sensitive device. According to the invention, the sensitive section of an atmospheric neutron single event effect sensitive device in a real environment can be acquired to provide an important basis for protection and evaluation of airborne electronic equipment.

Description

FOM is utilized to obtain method and the device in neutron single-particle effect device sensitivity cross section
Technical field
The present invention relates to microelectronics technology, particularly relate to a kind of method utilizing FOM acquisition neutron single-particle effect device sensitivity cross section and device.
Background technology
Place environment exists the high energy atmospheric neutron of 1MeV~1000MeV, air environment with storage organization complexity microelectronic component will necessarily meet with the high energy atmospheric neutron every about hour every square centimeter of 300~18000 1MeV~1000MeV in the place environment that flying height is 3000~20000 meters, produce single particle effect, thus affecting the reliability of electronic equipment. Device single particle effect sensitivity characteristic in Neutron Environment is characterized in the world with sensitive cross section. But, domestic but without the sensitive cross-section data under true environment at present, and flight test is relatively costly. Therefore, one of effectively evaluating device atmospheric neutron single particle effect sensitivity characteristic method is become by ground simulation test.
Domestic, the test pill that can be used for carrying out ground simulation test is 14MeV neutron emitter, but, owing to this neutron source is monoenergetic neutrons, and the energy of neutron is not monoenergetic under true environment, therefore, the sensitive cross section of simulation test gained Sensitive Apparatus that existing 14MeV neutron emitter carries out is utilized still to there is certain error with the sensitive cross section of true environment Sensitive Apparatus, sign Sensitive Apparatus sensitivity characteristic under true environment can not be directly used in, and then cause exactly Sensitive Apparatus in air environment to be carried out safety analysis.
Summary of the invention
For solving above-mentioned technical problem, the present invention proposes a kind of method utilizing FOM acquisition neutron single-particle effect device sensitivity cross section and device, by revising the test data of predetermined radiation source, obtain the sensitive cross section of atmospheric neutron single particle effect Sensitive Apparatus under true environment, and then air environment is met with high-energy neutron in place environment and carries out specific aim protection and evaluate by realization.
The invention provides a kind of method utilizing FOM acquisition neutron single-particle effect device sensitivity cross section, the method includes:
Adopt predetermined radiation source to carry out ground simulating, obtain the observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservation, and monitor the single particle effect number of errors N of Sensitive Apparatus in described simulation experimentend;
The Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor;
The Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor;
The value of modifying factor is calculated according to described first cofactor, the second cofactor and described single particle effect number of errors;
Value according to described modifying factor is to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationIt is modified.
Preferably, the described Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor, specifically include:
Obtain the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculate pre-setFOM;
Calculate the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the first cofactor.
Preferably, the described Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor, specifically include:
Obtain the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtain pre-setRosetta;
Calculate the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the second cofactor.
Preferably, the described value calculating modifying factor according to described first cofactor, the second cofactor and described single particle effect number of errors, specifically include:
Certainty of measurement computation model computational accuracy factor a according to sensitive cross section;
Calculate described first cofactor and the ratio of the second cofactor calculating, obtain accelerated factor Aβ;
According to described accelerated factor Aβ, dilution of precision a and described single particle effect number of errors calculate modifying factor A, formula is as follows:
A = A β ± a N end .
Preferably, described dilution of precision a is 1.96.
Preferably, the described value according to described modifying factor is to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationIt is modified, particularly as follows:
Calculate described modifying factor and the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationProduct, obtain the sensitive cross section σ of atmospheric neutron single particle effect Sensitive Apparatus0, formula is as follows:
σ0Observation×A。
Accordingly, the invention allows for a kind of device utilizing FOM acquisition neutron single-particle effect device sensitivity cross section, described device includes:
Acquisition module, is used for adopting predetermined radiation source to carry out ground simulating, obtains the observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservation, and obtain the single particle effect number of errors N of Sensitive Apparatus in the described simulation experiment monitoredend;
First computing module, the Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor;
Second computing module, for the Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor;
Modifying factor acquisition module, for calculating the value of modifying factor according to described first cofactor, the second cofactor and described single particle effect number of errors;
Correcting module, for the value according to described modifying factor to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationIt is modified.
Preferably, described first computing module includes:
First acquiring unit, for obtaining the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculate pre-setFOM;
First computing unit, for calculating the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the first cofactor.
Preferably, described second computing module includes:
Second acquisition unit, for obtaining the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtain pre-setRosetta;
Second computing unit, for calculating the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the second cofactor.
Preferably, described modifying factor acquisition module includes:
3rd computing unit, for the certainty of measurement computation model computational accuracy factor a according to sensitive cross section;
4th computing unit, for calculating described first cofactor and the ratio of the second cofactor calculating, obtains accelerated factor Aβ;
5th computing unit, for according to described accelerated factor Aβ, dilution of precision a and described single particle effect number of errors calculate modifying factor A, formula is as follows:
A = A β ± a N end .
The FOM that utilizes that the present invention proposes is adopted to obtain method and the device in neutron single-particle effect device sensitivity cross section, the method that make use of FOM, under the predetermined radiation source obtain test, the sensitive cross section of neutron single-particle effect Sensitive Apparatus is modified, obtain the sensitive cross section of atmospheric neutron single particle effect Sensitive Apparatus under true environment, obtain sensitivity accurately and take the fault rate of device, and then air environment is met with high-energy neutron in place environment and carries out specific aim protection and evaluate by realization.
Accompanying drawing explanation
Being more clearly understood from the features and advantages of the present invention by reference accompanying drawing, accompanying drawing is schematic and should not be construed as and the present invention is carried out any restriction, in the accompanying drawings:
Fig. 1 is a kind of method flow diagram utilizing FOM acquisition neutron single-particle effect device sensitivity cross section that the embodiment of the present invention one proposes;
Fig. 2 is a kind of apparatus module figure utilizing FOM acquisition neutron single-particle effect device sensitivity cross section that the embodiment of the present invention two proposes.
Detailed description of the invention
For making the purpose of the embodiment of the present invention, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the embodiment of the present invention, technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is a part of embodiment of the present invention, rather than whole embodiments. Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of protection of the invention.
Air environment with storage organization complexity microelectronic component will necessarily meet with the high energy atmospheric neutron every about hour every square centimeter of 300~18000 1MeV~1000MeV in the place environment of flying height (3000~20000 meters). these high-energy neutrons can penetrate cabin skin, beat in the kernel instruction control unit or critical data memory element of air environment, produce soft error and hard fault, cause navigation (navigation neceiver), radar-probing system (Connectors for Active Phased Array Radar), data network (the AFDX network switch), communication (optical fiber/bus), high speed computer system, avionic device, electromotor (FADEC), telex system, automatic Pilot technology, flight alarm, display screen, there is blank screen in other flight system etc. containing electronic device, crash, reset, restart, loss of data, the safety hazards such as order loss. in order to set up protection and appraisement system, it is necessary first to obtain the sensitive cross section of atmospheric neutron single particle effect Sensitive Apparatus under true environment. to this, the present invention proposes a kind of method utilizing FOM acquisition neutron single-particle effect device sensitivity cross section and device.
Fig. 1 is a kind of method flow diagram utilizing FOM acquisition neutron single-particle effect device sensitivity cross section that the embodiment of the present invention one proposes, as it is shown in figure 1, the method comprises the following steps:
S101, adopts predetermined radiation source to carry out ground simulating, obtains the observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservation, and monitor the single particle effect number of errors N of Sensitive Apparatus in described simulation experimentend
Preferably, the embodiment of the present invention adopt 14MeV neutron emitter as predetermined radiation source, the observation σ in Sensitive Apparatus sensitivity cross section under 14MeV neutron emitter radiatesObservationFor σ14MeV
Domestic carry out ground simulation test with the neutron emitter of 14MeV energy at present, to obtain sensitive cross-section data, in embodiments of the present invention, ground simulation test carries out irradiation by 14MeV neutron emitter, obtains the observation σ in Sensitive Apparatus sensitivity cross section under 14MeV neutron emitter radiates14MeV, by monitoring equipment writing task voltage and static current of lcd, retaking of a year or grade the single particle effect number of errors N of the Sensitive Apparatus of generation in testing with predose retaking of a year or grade Documents Comparison statistical simulationend
S102, the Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor.
S103, the Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor.
S104, calculates the value of modifying factor according to described first cofactor, the second cofactor and described single particle effect number of errors.
S105, according to the value of described modifying factor to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationIt is modified, particularly as follows: calculate described modifying factor and the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationProduct, obtain the sensitive cross section σ of atmospheric neutron single particle effect Sensitive Apparatus0, formula is as follows:
σ0Observation×A。
In embodiments of the present invention, adopt 14MeV neutron emitter as predetermined radiation source, the observation σ in Sensitive Apparatus sensitivity cross section under 14MeV neutron emitter radiatesObservationFor σ14MeV, step S102 will adopt the Sensitive Apparatus sensitivity cross section value σ that calculates of FOM methodFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor, specifically include: obtain the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculate pre-setFOM; Calculate the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under 14MeV neutron emitter radiates14MeVRatio, as the first cofactor A3, specific formula for calculation is:
A 3 = σ FOM σ 14 MeV
σ14MeV: the observation in the Sensitive Apparatus sensitivity cross section that 14MeV neutron emitter obtains. Unit: cm2/bit。
σFOM: utilize the Sensitive Apparatus cross section value that FOM method calculates. Unit: cm2/bit。
Charged particle in space radiation environment can cause the semiconductor device generation single particle effect in Spacecraft Electronic system, has a strong impact on reliability and the life-span of spacecraft. Single particle effect is that spacecraft occurs on space orbit, but substantial amounts of development test work carries out on ground. The foundation of the anti-single particle effect capability assessment of Spacecraft guidance and control required device is ground simulation test result. Current FOM (FigureofMerit, i.e. quality factor) method is to calculate the short-cut method of device single event upset rate in-orbit in ground simulation test, with according to limited device upset sensitivity parameter calculating device upset rate in-orbit conveniently and efficiently.
In embodiments of the present invention, adopt 14MeV neutron emitter as predetermined radiation source, the observation σ in Sensitive Apparatus sensitivity cross section under 14MeV neutron emitter radiatesObservationFor σ14MeV, step S103 will adopt the Sensitive Apparatus sensitivity cross section that the test of Rosetta true environment obtains to be worth σRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor, specifically include: obtain the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtain pre-setRosetta; Calculate the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under 14MeV neutron emitter radiates14MeVRatio, as the second cofactor A4, specific formula for calculation is:
A 4 = σ FOM σ Rosetta
σRosetta: the sensitive cross section value of the Sensitive Apparatus that the test of Rosetta true environment obtains, unit: cm2/bit。
In embodiments of the present invention, step S104 calculates the value of modifying factor according to described first cofactor, the second cofactor and described single particle effect number of errors, specifically includes:
Certainty of measurement computation model computational accuracy factor a according to sensitive cross section;
Calculate described first cofactor and the ratio of the second cofactor calculating, obtain accelerated factor Aβ, specific formula for calculation is:
A β = A 3 A 4
According to described accelerated factor Aβ, dilution of precision a and described single particle effect number of errors calculate modifying factor A, formula is as follows:
A = A β ± a N end .
Wherein, described dilution of precision a is 1.96.
For under unrepeatable sampling instances, significant level α=0.05, during confidence level CL=1-α=0.95, the definition according to confidence interval, then the certainty of measurement computation model in sensitive cross section is as follows:
Φ - 1 ( α 2 ) · 1 N · B - N B - 1 ≤ ϵ ---formula 1
Known:
B - N B - 1 ≈ 1 And Φ - 1 ( α 2 ) ≈ 1.96
Wherein, N is atmospheric neutron simple grain effect error sample quantity, unit: individual; B is atmospheric neutron single particle effect Sensitive Apparatus bit figure place, unit: individual; Described dilution of precision a is preferably 1.96.
Fig. 2 is a kind of apparatus module figure utilizing FOM acquisition neutron single-particle effect device sensitivity cross section that the embodiment of the present invention two proposes, as in figure 2 it is shown, described device includes:
Acquisition module 201, is used for adopting predetermined radiation source to carry out ground simulating, obtains the observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservation, and obtain the single particle effect number of errors N of Sensitive Apparatus in the described simulation experiment monitoredend;
First computing module 202, the Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor;
Second computing module 203, for the Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor;
Modifying factor acquisition module 204, for calculating the value of modifying factor according to described first cofactor, the second cofactor and described single particle effect number of errors;
Correcting module 205, for the value according to described modifying factor to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiates14MeVIt is modified.
The embodiment of the present invention adopt 14MeV neutron emitter as predetermined radiation source, the observation σ in Sensitive Apparatus sensitivity cross section under 14MeV neutron emitter radiatesObservationFor σ14MeV
The first computing module 202 in the embodiment of the present invention includes:
First acquiring unit, for obtaining the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculate pre-setFOM;
First computing unit, for calculating the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the first cofactor.
The second computing module 203 in the embodiment of the present invention includes:
Second acquisition unit, for obtaining the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtain pre-setRosetta;
Second computing unit, for calculating the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the second cofactor.
Modifying factor acquisition module 204 in the embodiment of the present invention includes:
3rd computing unit, for the certainty of measurement computation model computational accuracy factor a according to sensitive cross section;
4th computing unit, for calculating described first cofactor and the ratio of the second cofactor calculating, obtains accelerated factor Aβ;
5th computing unit, for according to described accelerated factor Aβ, dilution of precision a and described single particle effect number of errors calculate modifying factor A, formula is as follows:
A = A β ± a N end .
What the present invention proposed utilizes FOM to obtain method and the device in neutron single-particle effect device sensitivity cross section, has the advantages that
Instant invention overcomes the problem that the sensitive cross section of simulation test gained Sensitive Apparatus utilizing domestic existing predetermined radiation source to carry out exists certain error with the sensitive cross section of true environment Sensitive Apparatus, by the method utilizing existing FOM, under the predetermined radiation source obtain test, the sensitive cross section of neutron single-particle effect Sensitive Apparatus is modified, obtain the sensitive cross section of atmospheric neutron single particle effect Sensitive Apparatus under true environment, obtain sensitivity accurately and take the fault rate of device, and then air environment is met with high-energy neutron in place environment and carries out specific aim protection and evaluate by realization.
Through the above description of the embodiments, those skilled in the art is it can be understood that can realize by hardware to the present invention, it is also possible to the mode adding necessary general hardware platform by software realizes. Based on such understanding, technical scheme can embody with the form of software product, it (can be CD-ROM that this software product can be stored in a non-volatile memory medium, USB flash disk, portable hard drive etc.) in, including some instructions with so that a computer equipment (can be personal computer, server, or the network equipment etc.) performs the method described in each embodiment of the present invention.
It will be appreciated by those skilled in the art that accompanying drawing is the schematic diagram of a preferred embodiment, module or flow process in accompanying drawing are not necessarily implemented necessary to the present invention.
It will be appreciated by those skilled in the art that the module in the device in embodiment can describe according to embodiment to carry out being distributed in the device of embodiment, it is also possible to carry out respective change and be disposed other than in one or more devices of the present embodiment. The module of above-described embodiment can merge into a module, it is also possible to is further split into multiple submodule.
The several specific embodiments being only the present invention disclosed above, but, the present invention is not limited to this, and the changes that any person skilled in the art can think of all should fall into protection scope of the present invention.

Claims (10)

1. one kind utilizes the FOM method obtaining neutron single-particle effect device sensitivity cross section, it is characterised in that including:
Adopt predetermined radiation source to carry out ground simulating, obtain the observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservation, and monitor the single particle effect number of errors N of Sensitive Apparatus in described simulation experimentend;
The Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor;
The Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor;
The value of modifying factor is calculated according to described first cofactor, the second cofactor and described single particle effect number of errors;
Value according to described modifying factor is to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationIt is modified.
2. method according to claim 1, it is characterised in that the described Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor, specifically include:
Obtain the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculate pre-setFOM;
Calculate the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the first cofactor.
3. method according to claim 1, it is characterised in that the described Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor, specifically include:
Obtain the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtain pre-setRosetta;
Calculate the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the second cofactor.
4. method according to claim 1, it is characterised in that the described value calculating modifying factor according to described first cofactor, the second cofactor and described single particle effect number of errors, specifically includes:
Certainty of measurement computation model computational accuracy factor a according to sensitive cross section;
Calculate described first cofactor and the ratio of the second cofactor calculating, obtain accelerated factor Aβ;
According to described accelerated factor Aβ, dilution of precision a and described single particle effect number of errors calculate modifying factor A, formula is as follows:
A = A β ± a N end .
5. according to the arbitrary described method of claim 1-4, it is characterised in that described dilution of precision a is 1.96.
6. according to the arbitrary described method of claim 1-4, it is characterised in that the described value according to described modifying factor is to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationIt is modified, particularly as follows:
Calculate described modifying factor and the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationProduct, obtain the sensitive cross section σ of atmospheric neutron single particle effect Sensitive Apparatus0, formula is as follows:
σ0Observation×A。
7. one kind utilizes the FOM device obtaining neutron single-particle effect device sensitivity cross section, it is characterised in that described device includes:
Acquisition module, is used for adopting predetermined radiation source to carry out ground simulating, obtains the observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservation, and obtain the single particle effect number of errors N of Sensitive Apparatus in the described simulation experiment monitoredend;
First computing module, the Sensitive Apparatus sensitivity cross section value σ that FOM method will be adopted to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the first cofactor;
Second computing module, for the Sensitive Apparatus sensitivity cross section value σ that the test of Rosetta true environment will be adopted to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationCarry out division operation, obtain the second cofactor;
Modifying factor acquisition module, for calculating the value of modifying factor according to described first cofactor, the second cofactor and described single particle effect number of errors;
Correcting module, for the value according to described modifying factor to the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationIt is modified.
8. device according to claim 7, it is characterised in that described first computing module includes:
First acquiring unit, for obtaining the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculate pre-setFOM;
First computing unit, for calculating the described Sensitive Apparatus sensitivity cross section value σ adopting FOM method to calculateFOMWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the first cofactor.
9. device according to claim 7, it is characterised in that described second computing module includes:
Second acquisition unit, for obtaining the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtain pre-setRosetta;
Second computing unit, for calculating the described Sensitive Apparatus sensitivity cross section value σ adopting the test of Rosetta true environment to obtainRosettaWith the described observation σ in Sensitive Apparatus sensitivity cross section under predetermined radiation source radiatesObservationRatio, as the second cofactor.
10. device according to claim 7, it is characterised in that described modifying factor acquisition module includes:
3rd computing unit, for the certainty of measurement computation model computational accuracy factor a according to sensitive cross section;
4th computing unit, for calculating described first cofactor and the ratio of the second cofactor calculating, obtains accelerated factor Aβ;
5th computing unit, for according to described accelerated factor Aβ, dilution of precision a and described single particle effect number of errors calculate modifying factor A, formula is as follows:
A = A β ± a N end .
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CN112765869A (en) * 2021-01-05 2021-05-07 北京航空航天大学 Event rate estimation method integrating complete cross section and modified energy spectrum model

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