CN105893663A - Tri-strapdown inertial measurement unit non-quantization dynamic threshold value interval estimation method - Google Patents
Tri-strapdown inertial measurement unit non-quantization dynamic threshold value interval estimation method Download PDFInfo
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Abstract
The invention provides a tri-strapdown inertial measurement unit non-quantization dynamic threshold value interval estimation method. According to the specific scheme, the method includes the steps that 1, trajectory data with a tri-strapdown inertial measurement unit error model is generated through a Monte Carlo shooting method to serve as sample data; 2, the sample data is subjected to a normal distribution test, if the sample data conforms to normal distribution, the step 3 is executed, or else, it is shown that the sample data does not conform to normal distribution, and the method is withdrawn; 3, the threshold value confidence interval is estimated. Compared with a traditional method, normal distribution verification can be more precisely achieved, threshold value design is more reasonable, the threshold value confidence interval can be rapidly estimated, and simulated flight efficiency can be improved.
Description
Technical field
The invention belongs to the guidance of large-scale vehicle highly reliable flight navigation and control field, relate to a kind of three strapdowns
Used group non-quantized dynamic threshold method of interval estimation.
Background technology
Reliability, safety are had higher requirement by following Large Launch Vehicle.Control system is as fortune
Carry the nerve centre of rocket, the performance of whole carrier rocket is had very important effect.Strapdown inertial measurement unit is
The important component part of Guidance and control, carries out Redundancy Design to it and can be greatly improved reliability.
For three strapdown inertial measurement unit redundant systems, the design of threshold value is the pith of redundant system design,
Dynamically, while rational threshold design method can ensure ease for use as far as possible, improve reliability.Currently,
Needed for non-quantized dynamic threshold method for designing, sample is mostly based on tradition normal distribution-test method, it is impossible to accurately
Realize normal distribution checking, threshold design has certain deviation.
Summary of the invention
The technical problem to be solved is: overcome the deficiencies in the prior art, it is provided that a kind of three strapdowns are used to
Group non-quantized dynamic threshold method of interval estimation, solving non-quantized dynamic threshold method for designing needs accurately
The problem realizing normal distribution checking.
The present invention includes following technical scheme: a kind of three strapdown inertial measurement unit non-quantized dynamic threshold method of interval estimation,
Step is as follows:
1) ballistic data is generated
The ballistic data with three strapdown inertial measurement unit error models will be generated as sample by Monte-Carlo method method
Notebook data;
2) sample data is carried out normal distribution-test
21) to step 1) sample data that obtains carries out ascending sort according to numerical values recited, by all of
Sample data is divided into N group, and the sample data number often organized is Mi, i=1,2 ... N represents i-th group;ximax
Represent the data value that in i-th group, sample data is maximum, ximinRepresent the data value that in i-th group, sample data is minimum;Represent the estimation statistical average of i-th group of sample data;niRepresent i-th group of sample number
According to data amount check;N represents the total number of sample data;
22) below equation is utilized to try to achieve averageAnd variance
23) set the average of normal distribution, variance is respectively μ and variances sigma2, whenAnd
Time, represent sample data Normal Distribution, enter step 3);Otherwise show that sample data disobeys normal state
Distribution;Exit this method;Wherein A, B are threshold value;
3) threshold value Estimating Confidence Interval is carried out
The distribution density of overall X normal distribution is:
Solve the inverse function of standard normal distribution, obtain xmax、xmin, finally give threshold interval (xmax,
xmin)。
The present invention compared with prior art has the advantage that
(1) by step 2) smoothing processing to sample data, normal distribution can be realized more accurately and test
Card, makes threshold design more reasonable;
(2) to meeting the sample data of normal distribution, by step 3) threshold value confidence district can be rapidly completed
Between estimate, improve simulated flight efficiency.
Accompanying drawing explanation
Fig. 1 is a kind of non-quantized dynamic threshold method for designing flow chart.
Detailed description of the invention
The most just combine accompanying drawing the present invention is described further.
Below in conjunction with accompanying drawing, the present invention is described in more detail.Specifically include that
1. generation ballistic data:
The ballistic data with three strapdown inertial measurement unit error models will be generated as sample by Monte-Carlo method method
Notebook data;
2. pair sample data carries out normal distribution-test
21) to step 1) sample data that obtains carries out ascending sort according to numerical values recited, by all of sample
Notebook data is divided into N group, and the sample data number often organized is Mi, i=1,2 ... N represents i-th group;ximaxTable
Show the data value that in i-th group, sample data is maximum, ximinRepresent the data value that in i-th group, sample data is minimum;Represent the estimation statistical average of i-th group of sample data;niRepresent i-th group of sample number
According to data amount check;N represents that total number of samples is according to number;
22) below equation is utilized to try to achieve averageAnd variance
23) set the average of normal distribution, variance is respectively μ and variances sigma2, whenAndTime,
Represent sample data Normal Distribution, enter step 3);Otherwise show that sample data disobeys normal distribution;
Exit this method;Wherein A, B are threshold value;
3. carry out threshold value Estimating Confidence Interval
The distribution density of overall X normal distribution is:
Solve the inverse function of standard normal distribution, obtain xmax、xmin, finally give threshold interval (xmax,
xmin)。
The content not being described in detail in description of the invention belongs to existing known to professional and technical personnel in the field
Technology.
Claims (1)
1. a strapdown inertial measurement unit non-quantized dynamic threshold method of interval estimation, it is characterised in that step is as follows:
1) ballistic data is generated
The ballistic data with three strapdown inertial measurement unit error models will be generated as sample by Monte-Carlo method method
Notebook data;
2) sample data is carried out normal distribution-test
21) to step 1) sample data that obtains carries out ascending sort according to numerical values recited, by all of
Sample data is divided into N group, and the sample data number often organized is Mi, i=1,2 ... N represents i-th group;ximax
Represent the data value that in i-th group, sample data is maximum, ximinRepresent the data value that in i-th group, sample data is minimum;Represent the estimation statistical average of i-th group of sample data;niRepresent i-th group of sample number
According to data amount check;N represents the total number of sample data;
22) below equation is utilized to try to achieve averageAnd variance
23) set the average of normal distribution, variance is respectively μ and variances sigma2, whenAnd
Time, represent sample data Normal Distribution, enter step 3);Otherwise show that sample data disobeys normal state
Distribution;Exit this method;Wherein A, B are threshold value;
3) threshold value Estimating Confidence Interval is carried out
The distribution density of overall X normal distribution is:
Solve the inverse function of standard normal distribution, obtain xmax、xmin, finally give threshold interval (xmax,
xmin)。
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CN201610192259.XA CN105893663B (en) | 2016-03-30 | 2016-03-30 | A kind of non-quantized dynamic threshold method of interval estimation of three strapdown inertial measurement units |
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CN105893663A true CN105893663A (en) | 2016-08-24 |
CN105893663B CN105893663B (en) | 2019-06-18 |
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Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1851406A (en) * | 2006-05-26 | 2006-10-25 | 南京航空航天大学 | Gasture estimation and interfusion method based on strapdown inertial nevigation system |
CN103471613A (en) * | 2013-07-29 | 2013-12-25 | 南京航空航天大学 | Parameter simulation method for inertial navigation system of aircraft |
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2016
- 2016-03-30 CN CN201610192259.XA patent/CN105893663B/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1851406A (en) * | 2006-05-26 | 2006-10-25 | 南京航空航天大学 | Gasture estimation and interfusion method based on strapdown inertial nevigation system |
CN103471613A (en) * | 2013-07-29 | 2013-12-25 | 南京航空航天大学 | Parameter simulation method for inertial navigation system of aircraft |
Non-Patent Citations (1)
Title |
---|
王易南 等: "三捷联惯组冗余系统故障检测阈值设计方法", 《固体火箭技术》 * |
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