CN108254208B - A kind of simulator data creation method for aircraft complete machine test stand - Google Patents
A kind of simulator data creation method for aircraft complete machine test stand Download PDFInfo
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Abstract
The invention belongs to aircraft complete machines and system-level ground experiment technical field, are related to a kind of simulator data creation method for aircraft complete machine test stand.The present invention provides a kind of simulator data creation methods for aircraft complete machine test stand, the degree of automation of system-level ground experiment can be improved, so that the essential simulator for simulated flight device status information of system-level ground experiment is automatically controlled；The present invention may make big system test to be associated with Aeroplane control test by same ground simulation flight packet, to realize the linkage of big systems test bed Yu Aeroplane control test platform；The present invention can be not only used for aviation field, the fields such as the development, maintenance, inspection of other complication systems can equally be applied transformations to, such as the higher industrial circle convenient for information collection of the degree of automation such as space flight, ship, automobile, land transport device, there is biggish practical application value.
Description
Technical Field
The invention belongs to the technical field of aircraft complete machine and system level ground tests, and relates to a simulator data generation method for an aircraft complete machine test bed.
Background
In the overall aircraft and system-level ground test, a part of state information (such as height information and initiating explosive device action feedback) which is difficult to realize under the condition of a test room (such as an engine state) or difficult to simulate by using a real part needs to be simulated by an aircraft peripheral simulator. In the prior large-system ground test (without flight control), the aircraft peripheral simulators are controlled manually, so that the test operation is limited by manual information transmission, the test cannot be separated from a static operation mode, the simulator state adjustment is unrelated to the flight control, and the full-system operation state cannot be simulated together with the flight control in the ground test.
Disclosure of Invention
The purpose of the invention is as follows: aiming at the defects of the prior art, the simulator data generation method for the complete machine test bed of the aircraft is provided, and is used for generating simulator control data through a ground simulation flight packet and sending the simulator control data to the simulator, so that the requirements of dynamic testing of a ground test depending on an aircraft state simulator and ground test in linkage with a flight control system are met.
The technical scheme of the invention is as follows: the aircraft complete machine test bed comprises a flight control test bed, a large system test bed, an aircraft peripheral state simulator and a to-be-tested aircraft system, and is characterized in that the flight control test bed and the large system test bed are connected with a simulator data generation system by adopting flight bag resolving, and the simulator data generation method specifically comprises the following steps:
step 1, receiving flight bag data by a flight bag resolving and simulator data generating system: acquiring a ground simulation flight bag from a flight control test bed, and analyzing according to the communication format of the ground simulation flight bag of the flight control test bed to obtain simulation flight bag parameters;
step 2, acquiring and setting flight bag parameter time by a flight bag resolving and simulator data generation system: acquiring relative time information from the simulated flight packet parameters, and acquiring absolute time information from a large system test bed;
step 3, flight bag calculation and simulator data generation system calculation parameters: inputting the simulated flight bag parameters obtained by analyzing the communication format into a simulator data resolving model in the flight bag resolving and simulator data generating system, analyzing the parameters, and analyzing the obtained simulator control parameters;
step 4, recording flight bag data by a flight bag resolving and simulator data generating system: storing the flight control test bed ground simulation flight packet and simulation flight packet parameters obtained through communication format analysis by taking absolute time information and relative time information as indexes, and establishing the indexes in a database;
step 5, the flight bag resolving and simulator data generating system distributes simulator data: classifying the obtained simulator control parameters according to a sending target, and sending the simulator control parameters to a target simulator according to a target frequency;
step 6, the flight bag resolving and simulator data generating system monitoring control result: the flight bag resolving and simulator data generating system acquires controlled information fed back by the aircraft peripheral state simulator, and monitors transmission effectiveness of simulator control parameters, the working state of the aircraft peripheral state simulator and the controlled and executed conditions of the aircraft peripheral state simulator;
step 7, the flight bag resolving and simulator data generating system processes abnormal states: when the monitoring condition to aircraft peripheral state simulator goes wrong, handle according to the problem processing grade that aircraft complete machine test bench set for, the treatment includes: ignoring, retransmitting, suspending transmission and reporting accidents; and when the monitoring condition of the aircraft peripheral state simulator is not problematic, the steps 1 to 7 are circulated until the test is finished.
The specific steps of the simulator data generation method may also be as follows:
step 1, acquiring flight bag data by a flight bag resolving and simulator data generating system: inputting a ground simulation flight bag into a flight bag resolving and simulator data generating system, and analyzing according to the communication format of the ground simulation flight bag of the flight control test bed to obtain simulation flight bag parameters;
step 2, acquiring and setting flight bag parameter time by a flight bag resolving and simulator data generation system: acquiring relative time information from the simulated flight packet parameters, and acquiring absolute time information from a large system test bed;
step 3, flight bag calculation and simulator data generation system calculation parameters: inputting the simulated flight bag parameters obtained by analyzing the communication format into a simulator data resolving model in the flight bag resolving and simulator data generating system, analyzing the parameters, and analyzing the obtained simulator control parameters;
step 4, recording flight bag data by a flight bag resolving and simulator data generating system: storing the flight control test bed ground simulation flight packet and simulation flight packet parameters obtained through communication format analysis by taking absolute time information and relative time information as indexes, and establishing the indexes in a database;
step 5, the flight bag resolving and simulator data generating system distributes simulator data: classifying the obtained simulator control parameters according to a sending target, and sending the simulator control parameters to a target simulator according to a target frequency;
step 6, the flight bag resolving and simulator data generating system monitoring control result: the flight bag resolving and simulator data generating system acquires controlled information fed back by the aircraft peripheral state simulator, and monitors transmission effectiveness of simulator control parameters, the working state of the aircraft peripheral state simulator and the controlled and executed conditions of the aircraft peripheral state simulator;
step 7, the flight bag resolving and simulator data generating system processes abnormal states: when the monitoring condition to aircraft peripheral state simulator goes wrong, handle according to the problem processing grade that aircraft complete machine test bench set for, the treatment includes: ignoring, retransmitting, suspending transmission and reporting accidents; and when the monitoring condition of the aircraft peripheral state simulator is not problematic, the steps 1 to 7 are circulated until the test is finished.
In step 2, the clock information obtained from the flight bag is used as the relative time unified with the ground simulation flight bag, and may be the time information of any starting point, or the acceleration and deceleration time information, and the absolute time information obtained from the large system test bed is used as the absolute time, and is the time information synchronized with the local time.
In the step 3, the simulator control parameters obtained by analyzing the simulator data calculation model in the flight bag calculation and simulator data generation system are sent if the result is updated, and the simulator control parameters are sent in a unified manner without waiting for the completion of all parameter analysis.
In the step 5, an independent communication protocol is provided between the flight bag resolving and simulator data generating system and each aircraft peripheral state simulator, and each aircraft peripheral state simulator is independently controlled.
The internal functional modules of the flight bag resolving and simulator data generating system comprise: the method comprises the steps of flight bag receiving and format analysis, flight bag editing and sending queue management, relative absolute time setting, simulator control parameter calculation, data recording and storage and simulator control parameter sending, wherein,
the flight packet receiving and format analysis is used for receiving and format analysis of the ground simulation flight packet transmitted through the real-time data network;
the flight bag editing and sending queue management is used for self-setting editing and message queue management of the ground simulation flight bag, editing the contents of the ground simulation flight bag, generating a message queue, and setting sending frequency and repetition times;
the relative absolute time setting is used for managing relative time information acquired from the flight bag and absolute time information acquired from the local machine, clock information acquired from the flight bag is used as relative time unified with the flight bag, the relative time is time information of any starting point or acceleration and deceleration time information, and the time information acquired from the large system test stand is used as absolute time and is time information synchronous with local time;
resolving the control parameters of the simulator, inputting the simulated flight bag parameters obtained by analyzing the communication format into a simulator data resolving model in a flight bag resolving and simulator data generating system, analyzing the parameters, and analyzing the obtained simulator control parameters;
data storage and recording are to store the flight control test bed ground simulation flight packet and simulation flight packet parameters obtained through communication format analysis by taking absolute time information and relative time information as indexes, and establish the indexes in a database;
and sending the simulator control parameters, classifying the obtained simulator control parameters according to a sending target, and sending the simulator control parameters to the target simulator according to the target frequency.
A control option is arranged in the flight bag resolving and simulator data generating system, and the selection of taking the ground simulation flight bag obtained from the flight control test bed or recording the ground simulation flight bag is allowed.
The invention has the advantages and beneficial effects that:
1. the invention provides a simulator data generation method for an aircraft complete machine test bed, which can improve the automation degree of a system level ground test and automatically control a simulator which is necessary for the system level ground test and is used for simulating aircraft state information;
2. the control parameters of the simulator are resolved through a model based on a ground simulation flight bag, the conventional means of manually filling numerical values by means of signal electrical characteristics is changed, the data scientificity is higher, and the scientificity and effectiveness of test results are enhanced;
3. the invention can enable the large system test and the flight control test to be associated through the same ground simulation flight bag, thereby realizing the linkage of the large system test bed and the flight control test bed;
4. by the method, a test configuration supporting association with flight control can be constructed, so that test verification of a plurality of automatic system-level functions and fault modes in the configuration is supported;
5. the invention can provide an implementation idea for realizing linkage of the multi-system-level test bed.
The invention can be used in the aviation field, can also be used in the fields of development, maintenance, inspection and the like of other complex systems, such as the industrial fields of aerospace, ships, automobiles, land transporters and the like which have higher automation degree and are convenient for information acquisition, and has higher practical application value.
Drawings
FIG. 1 is a flow chart of a simulator data generation method for an aircraft complete machine test stand according to the present invention;
FIG. 2 is a diagram of a simulator data generation method for an aircraft complete machine test stand according to the present invention;
FIG. 3 is a sequence diagram illustrating the operation of a simulator data generating method for an aircraft complete machine test stand according to the present invention;
Detailed Description
The invention will be further explained with reference to the drawings.
The simulator data generation method for the complete machine test stand of the aircraft specifically comprises the following steps:
FIG. 1 illustrates the main steps of a simulator data generation method for an aircraft complete machine test stand according to the present invention. The method comprises the following steps:
the first step is that the flight bag resolving and simulator data generating system receives flight bag data: acquiring a ground simulation flight bag from a flight control test bed, and analyzing according to the communication format of the ground simulation flight bag of the flight control test bed to obtain simulation flight bag parameters;
secondly, acquiring and setting flight bag parameter time by a flight bag resolving and simulator data generation system: acquiring relative time information from the simulated flight packet parameters, and acquiring absolute time information from a large system test bed;
thirdly, flight bag resolving and simulator data generation system resolving parameters: inputting the simulated flight bag parameters obtained by analyzing the communication format into a simulator data resolving model in the flight bag resolving and simulator data generating system, analyzing the parameters, and analyzing the obtained simulator control parameters;
fourthly, recording the flight bag data by the flight bag resolving and simulator data generating system: storing the flight control test bed ground simulation flight packet and simulation flight packet parameters obtained through communication format analysis by taking absolute time information and relative time information as indexes, and establishing the indexes in a database;
fifthly, the flight bag resolving and simulator data generating system distributes simulator data: classifying the obtained simulator control parameters according to a sending target, and sending the simulator control parameters to a target simulator according to a target frequency;
sixthly, the flight bag resolving and simulator data generating system monitoring control result: the flight bag resolving and simulator data generating system acquires controlled information fed back by the aircraft peripheral state simulator, and monitors transmission effectiveness of simulator control parameters, the working state of the aircraft peripheral state simulator and the controlled and executed conditions of the aircraft peripheral state simulator;
and seventhly, processing the abnormal state by the flight bag resolving and simulator data generating system: when the monitoring condition to aircraft peripheral state simulator goes wrong, handle according to the problem processing grade that aircraft complete machine test bench set for, the treatment includes: ignoring, retransmitting, suspending transmission and reporting accidents; and when the monitoring condition of the aircraft peripheral state simulator is not problematic, circulating the first step to the seventh step until the test is finished.
FIG. 2 illustrates the internal structure of the flight bag calculation and simulator data generation system of the main operation system of the simulator data generation method for the complete machine test stand of the aircraft. The flight bag resolving and simulator data generating system is composed of a flight bag resolving module and a simulator data generating module.
The flight bag analysis module is mainly responsible for analyzing received ground simulation flight bag data into simulator control parameters, can locally input a simulation flight bag and edit a flight bag message queue under the condition that the external flight bag is not available, and sends the simulator control parameters obtained through analysis to the simulator data generation module through a network;
the simulator data generation module receives the parameters sent by the flight packet analysis module, performs counting verification, format verification, data analysis and content verification to obtain effective simulator control parameters, classifies the control parameters according to a sending target, sends control data to a target simulator according to a specific frequency, and simultaneously monitors and responds to the controlled state of the simulator.
The internal functional sub-modules of the simulator data generation module comprise: simulator control parameter receiving and format analysis, simulator control parameter editing and sending queue management, simulator control parameter classification and forwarding and the like. Wherein,
the simulator control parameter receiving and format analyzing device is used for acquiring simulator control parameters sent by the flight packet analyzing device, and performing counting verification, format verification, data analysis and content verification to obtain effective simulator control parameters;
the simulator control parameter editing and sending queue management is used for editing the simulator control parameters and managing the message queue customized by a user, the user can edit the content of the simulator control parameters to generate a message sending queue, and the sending frequency, the repetition times and the like can be set;
the simulator controls parameter classification and forwarding, realizes the classification of control parameters according to a sending target simulator, sends control data to the target simulator according to specific frequency, and simultaneously realizes the controlled state monitoring and accident handling of a controlled object.
The internal functional sub-modules of the simulator data generation module comprise: simulator control parameter receiving and format analysis, simulator control parameter editing and sending queue management, simulator control parameter classification and forwarding and the like. Wherein,
the simulator control parameter receiving and format analyzing device is used for acquiring simulator control parameters sent by the flight packet analyzing device, and performing counting verification, format verification, data analysis and content verification to obtain effective simulator control parameters;
the simulator control parameter editing and sending queue management is used for editing the simulator control parameters and managing the message queue customized by a user, the user can edit the content of the simulator control parameters to generate a message sending queue, and the sending frequency, the repetition times and the like can be set;
the simulator controls parameter classification and forwarding, realizes the classification of control parameters according to a sending target simulator, sends control data to the target simulator according to specific frequency, and simultaneously realizes the controlled state monitoring and accident handling of a controlled object.
The flight bag simulation module is provided with a control option which allows a user to select an external ground simulation flight bag or a self-editing flight bag;
the simulator data generation module has a control option that allows a user to select simulator control parameters or self-programming simulator control parameters from the flight bag simulation module.
Figure 3 illustrates the operational sequence of a simulator data generation method for an aircraft complete machine test stand according to the invention,
the grey part in the figure is simulator data generation method supporting equipment based on a simulation flight bag, the flight bag acquires the simulation flight bag from flight control test main control equipment, in view of real-time performance, the channel needs to be formed by adopting real-time transmission technologies such as a reflective memory and InfiniBand RDMA, the flight bag analyzes received flight bag data and resolves the flight bag data into simulator control parameters through a model and sends the simulator control parameters to simulator data generation, and the simulator data generation distributes simulator control data to each simulator according to configuration and set frequency.
As shown in the figure, the detailed operation flow of the simulator data generation method based on the simulated flight bag is as follows:
1) respectively starting the analysis of the flight bag and the generation of simulator data to complete initialization;
2) the simulator data generation starts to send control parameters to the simulator according to default data, generally sending the control parameters at a fixed frequency, so that the simulator is easy to judge the online state of the simulator data generation, and the simulator can be in a remote (externally controlled) or local (not externally controlled) state;
3) the simulator data generation and the simulator perform message response and state judgment according to the communication protocol;
4) the flight packet analysis receives the simulated flight packet information sent by the flight control test master control, and format analysis and caching are carried out on the information;
5) the flight bag analysis sends flight bag parameters into a pre-edited analysis model for parameter analysis;
6) sending the control parameters of a certain simulator after the analysis of the control parameters of the simulator is finished, and not waiting for the analysis of all the control parameters to be finished, but sending the control parameters not higher than a certain set frequency (generally 50Hz) in consideration of the load capacity of hardware;
7) simulator data generation receives the simulator control parameter, identifies the simulator corresponding to the parameter according to the frame format information, and forwards the packet parameter to the simulator.
Various modifications, variations and alternatives to the above-described method of the invention may occur to those skilled in the art, but fall within the scope of the invention as defined by the appended claims.
Claims (7)
1. A simulator data generation method for an aircraft complete machine test bed comprises a flight control test bed, a large system test bed, an aircraft peripheral state simulator and a to-be-tested aircraft system, and is characterized in that the flight control test bed and the large system test bed are connected with the simulator data generation system through flight bag resolving, and the simulator data generation method specifically comprises the following steps:
step 1, receiving flight bag data by a flight bag resolving and simulator data generating system: acquiring a ground simulation flight bag from a flight control test bed, and analyzing according to the communication format of the ground simulation flight bag of the flight control test bed to obtain simulation flight bag parameters;
step 2, acquiring and setting flight bag parameter time by a flight bag resolving and simulator data generation system: acquiring relative time information from the simulated flight packet parameters, and acquiring absolute time information from a large system test bed;
step 3, flight bag calculation and simulator data generation system calculation parameters: inputting the simulated flight bag parameters obtained by analyzing the communication format into a simulator data resolving model in the flight bag resolving and simulator data generating system, analyzing the parameters, and analyzing the obtained simulator control parameters;
step 4, recording flight bag data by a flight bag resolving and simulator data generating system: storing the flight control test bed ground simulation flight packet and simulation flight packet parameters obtained through communication format analysis by taking absolute time information and relative time information as indexes, and establishing the indexes in a database;
step 5, the flight bag resolving and simulator data generating system distributes simulator data: classifying the obtained simulator control parameters according to a sending target, and sending the simulator control parameters to a target simulator according to a target frequency;
step 6, the flight bag resolving and simulator data generating system monitoring control result: the flight bag resolving and simulator data generating system acquires controlled information fed back by the aircraft peripheral state simulator, and monitors transmission effectiveness of simulator control parameters, the working state of the aircraft peripheral state simulator and the controlled and executed conditions of the aircraft peripheral state simulator;
step 7, the flight bag resolving and simulator data generating system processes abnormal states: when the monitoring condition to aircraft peripheral state simulator goes wrong, handle according to the problem processing grade that aircraft complete machine test bench set for, the treatment includes: ignoring, retransmitting, suspending transmission and reporting accidents; and when the monitoring condition of the aircraft peripheral state simulator is not problematic, the steps 1 to 7 are circulated until the test is finished.
2. The method for generating simulator data for an aircraft complete machine test stand according to claim 1,
step 1, acquiring flight bag data by a flight bag resolving and simulator data generating system: and recording the ground simulation flight bag in the flight bag resolving and simulator data generating system, and analyzing according to the communication format of the ground simulation flight bag of the flight control test bed to obtain the simulation flight bag parameters.
3. The method for generating simulator data for an aircraft complete machine test bench according to claim 1 or 2, characterized in that in step 2, the clock information obtained from the flight bag is used as the relative time unified with the ground simulation flight bag, and can be the time information of any starting point, and also can be the acceleration and deceleration time information, and the absolute time information obtained from the large system test bench is used as the absolute time, and is the time information synchronized with the local time.
4. The method for generating the simulator data for the complete aircraft test stand according to claim 1 or 2, wherein in the step 3, the flight bag resolves the simulator control parameters obtained by analyzing the simulator data resolving model in the simulator data generating system, and if the result is updated, the result is sent, and the result is not sent uniformly after all parameters are resolved.
5. The method for generating simulator data for the complete aircraft test bench according to claim 1 or 2, wherein in the step 5, an independent communication protocol is provided between the flight bag calculation and simulator data generation system and each aircraft peripheral state simulator, so as to independently control each aircraft peripheral state simulator.
6. The method for generating simulator data for the complete aircraft test stand according to claim 1 or 2, wherein the flight bag calculation and simulator data generation system internal function module comprises: the method comprises the following steps of flight bag receiving and format analysis, flight bag editing and sending queue management, relative absolute time setting, simulator control parameter resolving, data recording and storage and simulator control parameter sending, wherein the flight bag receiving and format analysis is used for receiving and format analysis of a ground simulation flight bag transmitted through a real-time data network; the flight bag editing and sending queue management is used for self-setting editing and message queue management of the ground simulation flight bag, editing the contents of the ground simulation flight bag, generating a message queue, and setting sending frequency and repetition times;
the relative absolute time setting is used for managing relative time information acquired from the flight bag and absolute time information acquired from the local machine, clock information acquired from the flight bag is used as relative time unified with the flight bag, the relative time is time information of any starting point or acceleration and deceleration time information, and the time information acquired from the large system test stand is used as absolute time and is time information synchronous with local time;
resolving the control parameters of the simulator, inputting the simulated flight bag parameters obtained by analyzing the communication format into a simulator data resolving model in a flight bag resolving and simulator data generating system, analyzing the parameters, and analyzing the obtained simulator control parameters;
data storage and recording are to store the flight control test bed ground simulation flight packet and simulation flight packet parameters obtained through communication format analysis by taking absolute time information and relative time information as indexes, and establish the indexes in a database;
and sending the simulator control parameters, classifying the obtained simulator control parameters according to a sending target, and sending the simulator control parameters to the target simulator according to the target frequency.
7. The method as claimed in claim 1 or 2, wherein the flight bag calculation and simulator data generation system has a control option allowing selection of access to the ground simulation flight bag obtained from the flight control test stand or entry of the ground simulation flight bag.
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| CN109164717B (en) * | 2018-09-05 | 2021-11-16 | 中国航空工业集团公司北京长城航空测控技术研究所 | System-level test control method combined with simulation flight bag |
| CN109407669B (en) * | 2018-11-23 | 2021-06-08 | 中国船舶科学研究中心（中国船舶重工集团公司第七0二研究所） | Control method of multilayer fault-tolerant self-propelled ship model |
| CN110160811B (en) * | 2019-04-11 | 2020-05-15 | 浙江大学 | Electric automobile battery cold drawing test system based on feedback control |
| CN112783004B (en) * | 2020-12-29 | 2023-01-13 | 中国航空工业集团公司西安飞机设计研究所 | Redundancy simulation system for flight control computer of high-level simulator |
| CN112937914B (en) * | 2021-03-08 | 2023-02-03 | 中国航空工业集团公司北京长城航空测控技术研究所 | Ground simulation instruction processing method for aircraft complete machine test |
| CN114383879B (en) * | 2022-01-11 | 2024-05-24 | 安胜（天津）飞行模拟系统有限公司 | Test method of second-order differential loop in flight simulator identification test guidance system |
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