CN112308371B - Management and control system and management and control method for typical test of airplane - Google Patents
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Abstract
The invention relates to the technical field of airplane tests, in particular to a typical airplane test management and control system and a management and control method thereof, wherein the system comprises rule maintenance and daily use, wherein the rule maintenance comprises a first identity authentication module, a rule base and a rule base maintenance module; the daily use comprises a second identity authentication module, an execution condition import module and a system management and control module; in the method, the rule maintenance is utilized to maintain the preposed work items of the managed typical test, and the daily use is utilized to complete the management and control of the current overhead typical test. Through the system and the control method thereof, the problems of long cleaning time consumption, high labor consumption and deviation from the real situation can be effectively solved.
Description
Technical Field
The invention relates to the technical field of airplane tests, in particular to a typical airplane test management and control system and a typical airplane test management and control method.
Background
The airplane ground power-on debugging is an extremely important link in the airplane general assembly link and also an important inspection before the airplane test flight, and is concerned with the realization of flight safety, quality and normal functions of all systems. At present, before various power-on debugging tests, state cleaning is required to be carried out so as to ensure the safety and feasibility of the tests. The cleaning mode is mainly carried out by paper files, the cleaning involves a lot of personnel, the time consumption is long, various typical tests consume 1.5-3 days, and the cleaning is often carried out in advance for several days in order not to influence the production rhythm. Due to the fact that the cleaning period is long, the obtained cleaning conclusion usually deviates from the real situation, and therefore the accuracy of the start-up judgment of the typical test is influenced.
Disclosure of Invention
In order to solve the technical problems, the invention provides an airplane typical test management and control system and a management and control method thereof, which can effectively solve the problems of long cleaning time, much labor consumption and deviation from the real situation.
The invention is realized by adopting the following technical scheme:
the utility model provides a typical experimental management and control system of aircraft which characterized in that: including regular maintenance and daily use; the rule maintenance module comprises a first identity authentication module, a rule base and a rule base maintenance module; the first identity authentication module is used for verifying the identity of the process personnel in charge; the rule base is used for storing preposed working items of each typical test combed by a person in charge of the process according to the process flow; the rule base maintenance module is used for managing process personnel to update the rule base in time; the daily use comprises a second identity authentication module, an execution condition import module and a system management and control module; the second identity authentication module is used for verifying the identity of a user; the execution condition import module is used for importing the latest execution condition of the current rack; the system management and control module is used for judging the start-up of a typical test.
The specific process of rule maintenance comprises:
a. a process person in charge logs in through the first identity authentication module;
b. the process person in charge selects formal work needing to maintain the preposed work items in the rule base;
c. the process person in charge locates the position of formal work of the preposed work item to be maintained by searching;
d. the process personnel in charge maintain the preposed work items of the formal work;
e. and after the maintenance is finished, storing and exiting.
A management and control method of an aircraft typical test management and control system is characterized in that: the method comprises the following steps:
the process personnel in charge combs out typical test items according to the characteristics of the process production flow to form a typical test item set A: { a1, a2, … …, an };
and (II) according to the characteristics of the typical test, finishing and determining a preposed working set B: { b11, b12, … …, b1n }, each element in the set being a formal work number;
the user numbers the temporary work, wherein the temporary work number = formal work number + serial number; and establishing a corresponding work item set S according to the latest execution condition of the current rack by importing: { s1, s2, … …, sm };
extracting the latest work item set S as a data source S;
each element in the work item set S has x different execution states, the different execution states are scored with p, and the p =1, 2, … …, x is used for measuring the execution progress of work;
selecting a typical test ai needing attention, and determining a control state fraction p _ need of the prepositive work of the typical test ai, wherein the p _ need is a threshold value set by a process person in charge;
retrieving a work number containing a formal work number from the data source S according to the preposed work and typical test relation, checking the execution state of the element if the data source S contains the formal work number, and marking the element to pass if p is more than or equal to p _ need; if p < p _ need, the flag fails;
forming a new element set S 'with marks, checking the passing/failing marks of all elements in the new element set S', and executing a typical test ai if all the elements pass; if there are failed elements, the typical test ai may not be performed.
In the step eight, if the failed item exists, after the typical test ai is judged to be executable, the user can check the details of the failed item, including the number, the name and the execution unit of the failed item.
Logging in an account of erpandcheng before numbering the temporary work by a user; and after the corresponding work item set S is established, switching to a control account.
In the step (c), before the job number containing the official job number is retrieved from the data source S, each element containing the pre-job set B is retrieved one by one.
Compared with the prior art, the invention has the beneficial effects that:
1. in the prior art, the cleaning period is long, the system and the management and control method can complete the judgment result of the typical test start-up within several minutes by using the automatic system to introduce the latest current execution condition data in real time, and guarantee the timeliness of the cleaning state, thereby effectively realizing the management and control of the typical test.
2. In the system, a first identity authentication module is arranged in the rule maintenance, and a second identity authentication module is arranged in the daily use, so that the use safety is ensured. Logging in an erpandching account before the user numbers the temporary work; and after the corresponding work item set S is established, switching to a control account, and setting different management authorities for different information, so that the control method is more rigorous.
3. In the step (viii), if the failed element exists, after the typical test ai is determined to be unexecutable, the user can check details of the failed item, including the number, name and execution unit to which the failed item belongs, so that the user can determine the next work arrangement and centrally carry out the failed item work, thereby optimizing the typical test management and control.
4. In the step (c), before the data source S retrieves the work number containing the formal work number, each element containing the preposed work set B is retrieved one by one, so that the phenomena of omission and the like are avoided.
Drawings
The invention will be described in further detail with reference to the following description taken in conjunction with the accompanying drawings and detailed description, in which:
FIG. 1 is a schematic flow chart of the rule maintenance and daily use in the management and control system of the present invention;
FIG. 2 is a schematic diagram of a part of a process of the control method of the present invention;
FIG. 3 is a diagram illustrating the relationship between the pre-working set and the typical testing set in the present invention;
FIG. 4 is a schematic diagram showing the relationship change between the pre-working set and the typical testing set which change in real time according to the present invention;
FIG. 5 is a schematic diagram of the current rack execution scenario of the present invention;
FIG. 6 is a schematic diagram of an exemplary test management interface according to the present invention;
FIG. 7 is a schematic diagram of an exemplary pre-test workitem maintenance of the present invention;
FIG. 8 is a schematic diagram of the invention failing to pass a leading workitem;
FIG. 9 is a code diagram of an exemplary test management and control method of the present invention, FIG. 1;
FIG. 10 is a code diagram of an exemplary test management and control method of the present invention shown in FIG. 2;
fig. 11 is a code diagram 3 of an exemplary test management and control method according to the present invention.
Detailed Description
Example 1
As a basic implementation mode, the invention comprises a typical test management and control system of the airplane, which comprises regular maintenance and daily use. The rule maintenance module comprises a first identity authentication module, a rule base and a rule base maintenance module. The first identity authentication module is used for verifying the identity of the process personnel in charge. The rule base is used for storing preposed working items of each typical test which are combed by process personnel according to the process flow. And the rule base maintenance module is used for managing process personnel to update the rule base in time. The daily use comprises a second identity authentication module, an execution condition import module and a system management and control module. The second identity authentication module is used for verifying the identity of a user; the execution condition import module is used for importing the latest execution condition of the current shelf into a rule base. The system management and control module is used for judging the start of a typical test. The latest execution condition of the current rack comprises all formal work and temporary work execution conditions of the current rack, and each work has filed states such as not issued, issued and not dispatched, dispatched and not started, started and not completed, completed and not filed, and the like.
The rule maintenance establishes the control rule of the control system, and daily use is just to utilize the control rule to complete control. Once the rule maintenance is established, the maintenance is carried out only when the rule maintenance changes, and the use frequency is low; the daily use is according to user's demand, as conventional use, and the frequency of use is high.
Example 2
As a preferred embodiment of the invention, the invention comprises a typical test management and control system of an airplane, which is referred to the attached figure 1 of the specification and comprises regular maintenance and daily use. The rule maintenance is designed for the process personnel in charge, so that the rule maintenance is convenient for the personnel in charge to maintain the preposed work items of the typical test to be managed. The rule maintenance comprises a first identity authentication module, a rule base and a rule base maintenance module; the first identity authentication module is used for verifying the identity of the process personnel in charge; the rule base is used for storing preposed working items of each typical test combed by a person in charge of the process according to the process flow; and the rule base maintenance module is used for managing process personnel to update the rule base in time.
Lead items refer to the process steps that precede typical trials in the process flow and are a prerequisite to typical trials. And (4) combing the precondition of each typical test by the process personnel in charge according to the process flow, and improving the precondition in the regular maintenance in time. The preposition work items in the rule maintenance are the key points of the whole typical test management and control system, and the correctness of the preposition work items directly determines the management and control quality. And if the process flow changes, the preposed work items are changed, the process personnel in charge update the rule maintenance module in time, and if the process flow does not change, the original state is maintained.
The specific process of rule maintenance comprises the following steps:
a. and the process personnel in charge logs in through the first identity authentication module.
b. And (3) the process person in charge selects formal work needing to maintain the preposed work items in the rule base, such as: the formal work of the main pipe of the process A is taken as A (every time of the work), the work which needs to be completed when the A is developed is called preposed work items, and when the preposed work items are changed, the fact that the formal work A needs maintenance is determined.
c. A supervisor process worker positions formal work positions of the preposed work items to be maintained through searching, specifically, pull-down items can be designed for the supervisor process worker, all formal work is covered, the formal work to be maintained is selected through pull-down, a determination button is clicked, and the system performs searching and positioning on the whole page according to the number characters of the formal work.
d. The process personnel in charge maintains the preposed work items of the formal work, and adds the preposed work item numbers if the preposed work items are increased with reference to the attached figure 7 of the specification; if the front work item is changed, the number of the front work item is changed.
e. And after the maintenance is finished, storing and exiting.
Daily use is designed to the user of service, and the user of service is convenient for to introduce the completion condition of current shelf number process to set for the management and control rule as required, thereby accomplish the experimental management and control of current shelf number typical. The daily use comprises a second identity authentication module, an execution condition import module and a system management and control module; the second identity authentication module is used for verifying the identity of a user; the execution condition import module is used for importing the latest execution condition of the current shelf into a rule base; the system management and control module is used for judging the start-up of a typical test.
The specific use flow of the daily use is as follows: and (4) logging in the account of erpandcheng by a user, importing the latest execution condition of the current frame according to a set format, and switching to the control account after the latest execution condition is finished. And (3) setting the completion degree of the preposed work item (such as 6 points filed, 5 points finished to be filed and the like) by using personnel according to needs, namely setting the judgment score of the preposed work item, and after the setting is finished, selecting a pre-developed test item by a user and clicking 'confirm'. The management and control system performs comparison analysis in the current execution situation of the shelf according to the evaluation score set by the user and the preposed work of the selected 'test item' (the preposed work of the process in charge of maintenance in the rule maintenance module). Judging the preposed working items more than or equal to the evaluation scores as passing items; the preposed work item which is smaller than the judgment score is judged as a failed test item; and (3) comprehensively selecting all the preposed working items of the test items, and if no failed item exists, drawing a conclusion that: the operation can be started; if there is a failed term, it is concluded: and the operation is not possible, so that the operation judgment is performed in a typical test. For the non-workable item, the user can further view the details of the failed item (including the number, name and execution unit of the failed item) through the "details". And the user can determine the next work arrangement according to the details of the failed items, and intensively carry out the failed item work, so that the typical test management and control are optimized. Taking a typical test as an example, the implementation code can refer to the specification, namely the attached figure 9-the attached figure 11.
Example 3
As the best implementation mode, the invention comprises a typical test management and control system of the airplane, which comprises regular maintenance and daily use; the rule maintenance module comprises a first identity authentication module, a rule base and a rule base maintenance module; the first identity authentication module is used for verifying the identity of the process personnel in charge; the rule base is used for storing preposed working items of each typical test combed by the process personnel according to the process flow; the rule base maintenance module is used for managing process personnel to update the rule base in time; the daily use comprises a second identity authentication module, an execution condition import module and a system management and control module; the second identity authentication module is used for verifying the identity of a user; the execution condition import module is used for importing the latest execution condition of the current frame into a rule base; the system management and control module is used for judging the start-up of a typical test.
The specific process of the rule maintenance comprises the following steps:
a. a process person in charge logs in through the first identity authentication module;
b. the process personnel in charge selects formal work needing to maintain the preposed work items in the rule base;
c. the process person in charge locates the position of formal work needing to maintain the preposed work items by searching;
d. the process personnel in charge maintain the preposed work items of the formal work;
e. and after the maintenance is finished, storing and exiting.
Based on the management and control system, the invention comprises a management and control method of an airplane typical test management and control system, which comprises the following steps:
the process personnel in charge combs out typical test items according to the characteristics of the process production flow to form a typical test item set A: { a1, a2, … …, an }. The process production flow is a main line of an aircraft manufacturing link, and a plurality of typical test items, namely key nodes, exist on the main line.
Within the collection of typical test items, the conditions under which each typical test item is performed are referred to as pre-work. According to the characteristics of a typical test, a front working set B is determined by sorting: { b11, b12, … …, b1n }, the front work of a typical test item is the core element of control, and each element in the set is a formal work number. The relation between the front working set and the typical test set can refer to the attached figure 3 of the specification.
Thirdly, because various factors exist in the whole aircraft process production flow: product failure, surface quality problems, equipment inspection and upgrading and the like. Several provisional jobs are generated from various factors. To build a reasonably and effectively governing rule, both formal and provisional work must be combined. Due to the fact that the execution condition of the airplane changes, the generated temporary work types are different, and the number of the temporary work types is different. The number of temporary operations of the same aircraft may change dynamically at different times. A user numbers temporary work, wherein the temporary work number = official work number + serial number; if the formal job number is b11, the corresponding provisional job numbers are b111 and b 112. The pre-job and typical test relationships vary for different periods of different stands, with particular reference to figure 4 of the specification. The work items corresponding to each shelf contain formal work and temporary work, and a user needs to import the latest execution condition of the current shelf into a module according to the import execution condition to form a real-time work item set S: { s1, s2, … …, sm }. Referring to the attached figure 5 of the specification, the current latest execution condition comprises the execution conditions of all formal works and temporary works of the current shelf, and the execution condition of each work comprises the states of unowned work, assigned work without dispatching, dispatched work without starting work, started work without finishing, finished work without filing and filed.
And fourthly, during specific management and control, referring to the attached figure 2 of the specification, the work item set S is in a dynamic change process, and the latest work item set S is extracted to serve as the data source S.
Each element in the work item set S has x different execution states, which respectively mark different execution stages of each element, and the different execution states are scored by p, where p =1, 2, … …, x is used to measure the execution progress of the work, for example: the first stage, p =1 point, the second stage, p = 2 point, … …, the xth stage, p = x point.
Selecting a typical test ai needing attention from the typical test set A, and determining a control state fraction p _ need of the prepositive work of the typical test ai, wherein the p _ need is a threshold value set by a process person in charge; the management and control personnel can carry out corresponding adjustment according to different requirements.
And (c) searching a work number containing a formal work number in a data source S according to the preposed work and typical test relation in the attached figure 3 of the specification, wherein the schematic diagram refers to the attached figure 4 of the specification. Taking the typical test a1 as an example, each element containing the pre-work set B is searched in the data source S item by item, the work containing the formal work number is searched, and whether the work passes or not is marked by using the judgment criterion that p is more than or equal to p _ need: if p is more than or equal to p _ need, the flag is passed; if p < p _ need, the flag is not passed.
Combining all marked elements to form a marked new element set S ', wherein the set S' comprises a working set B and temporary work derived from the working set B. Referring to fig. 6 of the specification, the pass/fail flag of all elements in the new element set S' is checked, and if all elements pass, a conclusion is reached: a typical test ai can be performed; if there are failed elements, the conclusion is reached: the typical test ai may not be performed. If there is a failed element, then after the typical test ai cannot be performed, the user can view the details of the failed item, including the number, name, and execution unit of the failed item, with reference to fig. 8 of the specification. And the user can determine the next work arrangement according to the details of the failed items, and intensively carry out the failed item work, so that the typical test management and control are optimized.
In summary, after reading the present disclosure, those skilled in the art should make various other modifications without creative efforts according to the technical solutions and concepts of the present disclosure, which are within the protection scope of the present disclosure.
Claims (5)
1. A management and control method of an aircraft typical test management and control system is characterized in that: the typical test management and control system of the airplane comprises regular maintenance and daily use; the rule maintenance module comprises a first identity authentication module, a rule base and a rule base maintenance module; the first identity authentication module is used for verifying the identity of the process personnel in charge; the rule base is used for storing preposed working items of each typical test combed by a person in charge of the process according to the process flow; the rule base maintenance module is used for managing process personnel to update the rule base in time; the daily use comprises a second identity authentication module, an execution condition import module and a system management and control module; the second identity authentication module is used for verifying the identity of a user; the execution condition import module is used for importing the latest execution condition of the current rack; the system management and control module is used for judging the start-up of a typical test;
the management and control method comprises the following steps:
the process personnel in charge combs out typical test items according to the characteristics of the process production flow to form a typical test item set A: { a1, a2, … …, an };
according to the characteristics of a typical test, a preposed working set B is determined by sorting: { b11, b12, … …, b1n }, each element in the set being a formal work number;
the user numbers the temporary work, wherein the temporary work number = formal work number + serial number; and establishing a corresponding work item set S according to the latest execution condition of the current frame by importing: { s1, s2, … …, sm };
extracting the latest work item set S as a data source S;
each element in the work item set S has x different execution states, the different execution states are scored with p, and the p =1, 2, … …, x is used for measuring the execution progress of work;
selecting a typical test ai needing attention, and determining a control state fraction p _ need of prepositive work of the typical test ai, wherein the p _ need is a threshold set by a process person in charge;
searching a work number containing a formal work number in the data source S according to the preposed work and typical test relation, checking the execution state of the element if the data source S contains the formal work number, and marking to pass if p is more than or equal to p _ ned; if p < p _ need, the flag fails;
forming a new element set S 'with marks, checking the passing/failing marks of all elements in the new element set S', and if all the elements pass, executing a typical test ai; if there are failed elements, then the typical test ai may not be performed.
2. The management and control method of the typical test management and control system of the airplane as claimed in claim 1, wherein: the specific process of rule maintenance comprises:
a. the process personnel in charge logs in through the first identity authentication module;
b. the process person in charge selects formal work needing to maintain the preposed work items in the rule base;
c. the process person in charge locates the position of formal work needing to maintain the preposed work items by searching;
d. the process person in charge maintains the preposed work items of the formal work;
e. and after the maintenance is finished, storing and exiting.
3. The management and control method of the aircraft typical test management and control system according to claim 1, characterized in that: in the step (viii), after determining that the typical test ai cannot be executed if the failed element exists, the user can view details of the failed item, including the number, name, and execution unit of the failed item.
4. The management and control method of the typical test management and control system of the airplane as claimed in claim 2 or 3, wherein: logging in an account of erpandcheng before numbering the temporary work by a user; and after the corresponding work item set S is established, switching to a control account.
5. The management and control method of the typical test management and control system of the airplane as claimed in claim 4, wherein: in the step (c), before the work number including the official work number is retrieved from the data source S, each element including the pre-work set B is retrieved one by one.
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