CN108922251A - A kind of TCASII airborne collision avoidance system flying platform flying quality limitation processing method and system - Google Patents
A kind of TCASII airborne collision avoidance system flying platform flying quality limitation processing method and system Download PDFInfo
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- CN108922251A CN108922251A CN201810871574.4A CN201810871574A CN108922251A CN 108922251 A CN108922251 A CN 108922251A CN 201810871574 A CN201810871574 A CN 201810871574A CN 108922251 A CN108922251 A CN 108922251A
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0004—Transmission of traffic-related information to or from an aircraft
- G08G5/0008—Transmission of traffic-related information to or from an aircraft with other aircraft
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0073—Surveillance aids
- G08G5/0078—Surveillance aids for monitoring traffic from the aircraft
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- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/04—Anti-collision systems
- G08G5/045—Navigation or guidance aids, e.g. determination of anti-collision manoeuvers
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- Computer Networks & Wireless Communication (AREA)
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- Emergency Alarm Devices (AREA)
Abstract
The present invention provides a kind of TCASII airborne collision avoidance system flying platform flying quality limitation processing method and systems, including parameter acquisition module, parameter processing module, parameter table look-up module, parameter selftest module and parameter to check setup module；Processing in real time is carried out to flight performance parameter and is updated in conjunction with TCASII airborne collision avoidance system core algorithm according to the real-time aeroplane performance of platform, to obtain real-time flying quality restricted information, provides real-time more accurate alarm.Make TCASII airborne collision avoidance system that there is better user experience, platform is enable to obtain the safety instruction more refined, makes TCASII airborne collision avoidance system with more the market competitiveness.
Description
Technical field
The present invention relates to a kind of TCASII airborne collision avoidance system flying platform flying quality limitation processing method and systems, relate to
And blank pipe anticollision field.
Background technique
TCASII is an airborne collision avoidance system, is mainly used for providing air security separation assurance for aircraft, reaches anti-collision
The purpose hit.By inquiry, reception, the recall signal for handling other aircraft answering machines, other aircrafts of surrounding are monitored,
And it calculates other aircrafts in monitoring range and provides traffic alert with respect to the flight trend of the machine and resolution alarm is suggested.
There are many function of TCASII airborne collision avoidance system itself, system composition and its complexity, in TCASII airborne collision avoidance system
Influence of the aeroplane performance to anticollision logic is defined in the minimum performance standards of system, and the aeroplane performance is needed to inform and be given
TCASII airborne collision avoidance system.
Current TCASII airborne collision avoidance system, according to the minimum performance standards of TCASII airborne collision avoidance system（RTCA/
DO-185A/ RTCA/DO-185B）It is designed, what wherein the limitation of aeroplane performance generallyd use is discrete lines design, in this way
The aircraft for some type will be will cause, once discrete lines determine, which can not will provide airborne collision avoidance system always
Certain alarms of system, and then influencing aeroplane performance cannot be mutually coordinated in real time with airborne collision avoidance system alarm, since aircraft is flat
There is no reactions in real time to give TCASII airborne collision avoidance system for the truth of platform, so that TCASII airborne collision avoidance system can not
The real-time input according to aircraft actual performance is realized utmostly to play the safety effect of TCASII airborne collision avoidance system.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of TCASII airborne collision avoidance system flying platform flying quality limits
Processing method and system processed have the characteristics that make to alert accuracy and real-time are higher.
A kind of TCASII airborne collision avoidance system flying platform flying quality limitation processing system, which is characterized in that including,
Parameter acquisition module, the flight performance parameter of platform where obtaining；The flight performance parameter include temperature, loading capacity and
The real-time parameter of height；
Parameter processing module carries out classification processing to the flight performance parameter of acquisition；
Parameter table look-up module tables look-up to the parameter that classification processing is crossed, and acquires the phase of TCASII airborne collision avoidance system needs
Flying quality limitation input parameter is closed, and parameter is sent to TCASII airborne collision avoidance system core logic；Wherein, for looking into
The table of inquiry is the airplane Performance Sheet extracted by the platform In-Flight Performance curve, while cooperating TCASII airborne collision avoidance system
The aeroplane performance that core algorithm needs limits parameter, the platform flight performance parameter inquiry table of establishment；
Parameter selftest module, the parameter self-test of the various influence platform flying qualitys of platform where completing, and save and report self-test
As a result TCASII airborne collision avoidance system central maintenance subsystem is given；
Parameter checks setup module, and real-time online inquires the platform flight performance parameter inquiry table, if flown in aircraft platform
Row performance curve changes, then modifies to parameter.
A kind of TCASII airborne collision avoidance system flying platform flying quality limitation processing method, in the base of above-mentioned processing system
It is realized on plinth, specific method includes,
S1, TCASII airborne collision avoidance system power on, and TCASII airborne collision avoidance system receives and dispatches host reading platform flight performance parameter
Inquiry table, and if so, the flight performance parameter inquiry table information of aircraft platform is saved and record, into S2；Otherwise, enter
S6；
S2 obtains aircraft platform flight performance parameter, and judges whether to obtain successfully, if obtained successfully, carries out S3；If obtained
Take it is unsuccessful, carry out repeat acquisition, repeat times of acquisition reach repetition times of acquisition threshold value, then report parameter obtain failure；
S3 detects aircraft platform flight performance parameter, if all normal, into S4, corresponding aircraft platform is otherwise reported to fly
Row performance parameter failure, into S2；
S4 carries out classification processing to aircraft platform flight performance parameter, into S5；
S5, start-up parameter table look-up module, to treated, aircraft platform flight performance parameter is tabled look-up, and it is airborne to obtain TCASII
The related flying quality limitation input parameter that anti-collision system core algorithm needs, and give the parameter to TCASII airborne collision avoidance system
Core algorithm of uniting is handled；Return to S2；
The platform flying quality limitation of S6, TCASII airborne collision avoidance system automatically processes subsystem and uses the aircraft defaulted in software
The flight performance parameter inquiry table of platform, and the flight performance parameter inquiry table of aircraft platform is automatically generated in FLASH, as
Power on use next time.
The method also includes using if detecting aircraft platform flight performance parameter failure in continuous N number of period S3
The aeroplane performance that TCASII airborne collision avoidance system tail portion discrete lines provide limits input；Wherein, N is the natural number more than or equal to 2.
The method also includes using TCASII airborne collision avoidance system if continuous N periodic report parameter obtains failure
The aeroplane performance that tail portion discrete lines of uniting provide limits input；Wherein, M is the natural number more than or equal to 1.
The method also includes when the aeroplane performance limitation provided using TCASII airborne collision avoidance system tail portion discrete lines is defeated
When entering also unavailable, aircraft platform flying quality is set without limitation.
The N is equal to 3.
The M is equal to 3.
The method of parameter query includes that the platform flight performance parameter inquiry table is solidificated in airborne collision avoidance processing software
In for inquiring.
The method of parameter query includes being solidificated in the platform flight performance parameter inquiry table in the form of configuration file
For inquiring in the FLASH of processing module where the anticollision core algorithm of TCASII airborne collision avoidance system.
Compared with prior art, the beneficial effects of the invention are as follows：Can according to the real-time aeroplane performance of platform, in conjunction with
TCASII airborne collision avoidance system core algorithm provides real-time more accurate alarm；There is TCASII airborne collision avoidance system more
Good user experience, enables platform to obtain the safety instruction more refined, makes TCASII airborne collision avoidance system with more city
Field competitiveness.
Detailed description of the invention
Fig. 1 is the system structure diagram of a wherein embodiment of the invention.
Fig. 2 is the processing flow schematic diagram of a wherein embodiment of the invention.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right
The present invention is further elaborated.It should be appreciated that described herein, specific examples are only used to explain the present invention, not
For limiting the present invention.
This specification（Including abstract and attached drawing）Disclosed in any feature unless specifically stated can be equivalent by other
Or the alternative features with similar purpose are replaced.That is, unless specifically stated, each feature is a series of equivalent or class
Like an example in feature.
As shown in Figure 1, a kind of TCASII airborne collision avoidance system flying platform flying quality limits processing system, including,
Parameter acquisition module, the flight performance parameter of platform where obtaining；The flight performance parameter include temperature, loading capacity and
The real-time parameter of height；
Parameter processing module carries out classification processing to the flight performance parameter of acquisition；
Parameter table look-up module tables look-up to the parameter that classification processing is crossed, and acquires the phase of TCASII airborne collision avoidance system needs
Flying quality limitation input parameter is closed, and parameter is sent to TCASII airborne collision avoidance system core logic；Wherein, for looking into
The table of inquiry is the airplane Performance Sheet extracted by the platform In-Flight Performance curve, while cooperating TCASII airborne collision avoidance system
The aeroplane performance that core algorithm needs limits parameter, the platform flight performance parameter inquiry table of establishment；
Parameter selftest module, the parameter self-test of the various influence platform flying qualitys of platform where completing, and save and report self-test
As a result TCASII airborne collision avoidance system central maintenance subsystem is given；
Parameter checks setup module, and real-time online inquires the platform flight performance parameter inquiry table, if flown in aircraft platform
Row performance curve changes, then modifies to parameter.
The present invention devises TCASII airborne collision avoidance system platform flight performance parameter interface, available by the interface
The parameter live data values of aircraft platform flying quality are influenced, guarantee the real-time flight situation that can obtain aircraft；It devises
TCASII airborne collision avoidance system S mode answering machine and the platform flight performance parameter of TCASII airborne collision avoidance system transmitting-receiving host connect
Mouthful, guarantee that the real-time flight performance parameter of aircraft platform can reach the platform flying quality limitation of TCASII airborne collision avoidance system
Automatically process subsystem；It devises online query or modifies the flight performance parameter inquiry table interface of aircraft platform, guarantee flying
When machine platform flying quality curve changes, it can modify according to the actual situation.
It is designed according to above-mentioned system, it can be convenient for handling the limitation of flying platform flying quality, so that alarm is more
Accurately, the safety instruction more refined.
As shown in Fig. 2, a kind of TCASII airborne collision avoidance system flying platform flying quality limits processing method, at above-mentioned place
It is realized on the basis of reason system, specific method includes,
S1, TCASII airborne collision avoidance system power on, and TCASII airborne collision avoidance system receives and dispatches host reading platform flight performance parameter
Inquiry table, and if so, the flight performance parameter inquiry table information of aircraft platform is saved and record, into S2；Otherwise, enter
S6；
S2 obtains aircraft platform flight performance parameter, and judges whether to obtain successfully, if obtained successfully, carries out S3；If obtained
Take it is unsuccessful, carry out repeat acquisition, repeat times of acquisition reach repetition times of acquisition threshold value, then report parameter obtain failure；
S3 detects aircraft platform flight performance parameter, if all normal, into S4, corresponding aircraft platform is otherwise reported to fly
Row performance parameter failure, into S2；
S4 carries out classification processing to aircraft platform flight performance parameter, into S5；
S5, start-up parameter table look-up module, to treated, aircraft platform flight performance parameter is tabled look-up, and it is airborne to obtain TCASII
The related flying quality limitation input parameter that anti-collision system core algorithm needs, and give the parameter to TCASII airborne collision avoidance system
Core algorithm of uniting is handled；Return to S2；
The platform flying quality limitation of S6, TCASII airborne collision avoidance system automatically processes subsystem and uses the aircraft defaulted in software
The flight performance parameter inquiry table of platform, and the flight performance parameter inquiry table of aircraft platform is automatically generated in FLASH, as
Power on use next time.
The present invention, which solves TCASII airborne collision avoidance system, can not obtain the real-time aeroplane performance of aircraft platform, can only basis
The aeroplane performance discrete lines combination TCASII airborne collision avoidance system core algorithm that aircraft platform determines in advance provides the alarm of limitation
Type, the problem of optimal alarm can not being provided according to the flying quality of aircraft platform at that time in real time.It can be according to platform reality
When aeroplane performance provide real-time more accurate alarm in conjunction with TCASII airborne collision avoidance system core algorithm.Make TCASII machine
Carrying anti-collision system has better user experience, so that platform is obtained the safety instruction more refined, keeps TCASII airborne
Anti-collision system has more the market competitiveness.
As one embodiment of the present invention, the method also includes if detect aircraft in continuous N number of period S3
Platform flight performance parameter failure limits input using the aeroplane performance that TCASII airborne collision avoidance system tail portion discrete lines provide；
Wherein, N is the natural number more than or equal to 2.
As one embodiment of the present invention, the method also includes if continuous N periodic report parameter obtains event
Barrier then limits input using the aeroplane performance that TCASII airborne collision avoidance system tail portion discrete lines provide；Wherein, M is more than or equal to 1
Natural number.
As one embodiment of the present invention, the method also includes when use TCASII airborne collision avoidance system tail portion
When the aeroplane performance limitation input that discrete lines provide is also unavailable, aircraft platform flying quality is set without limitation.
As one embodiment of the present invention, the N is equal to 3.
As one embodiment of the present invention, the M is equal to 3.
As one embodiment of the present invention, the method for parameter query includes looking into the platform flight performance parameter
Inquiry table is solidificated in airborne collision avoidance processing software for inquiring.
As one embodiment of the present invention, the method for parameter query includes looking into the platform flight performance parameter
Inquiry table is solidificated in the FLASH of the processing module where the anticollision core algorithm of TCASII airborne collision avoidance system in the form of configuration file
In for inquiring.
Claims (9)
1. a kind of TCASII airborne collision avoidance system flying platform flying quality limits processing system, which is characterized in that including,
Parameter acquisition module, the flight performance parameter of platform where obtaining；The flight performance parameter include temperature, loading capacity and
The real-time parameter of height；
Parameter processing module carries out classification processing to the flight performance parameter of acquisition；
Parameter table look-up module tables look-up to the parameter that classification processing is crossed, and acquires the phase of TCASII airborne collision avoidance system needs
Flying quality limitation input parameter is closed, and parameter is sent to TCASII airborne collision avoidance system core logic；Wherein, for looking into
The table of inquiry is the airplane Performance Sheet extracted by the platform In-Flight Performance curve, while cooperating TCASII airborne collision avoidance system
The aeroplane performance that core algorithm needs limits parameter, the platform flight performance parameter inquiry table of establishment；
Parameter selftest module, the parameter self-test of the various influence platform flying qualitys of platform where completing, and save and report self-test
As a result TCASII airborne collision avoidance system central maintenance subsystem is given；
Parameter checks setup module, and real-time online inquires the platform flight performance parameter inquiry table, if flown in aircraft platform
Row performance curve changes, then modifies to parameter.
2. a kind of TCASII airborne collision avoidance system flying platform flying quality limits processing method, handled described in claim 1
It is realized on the basis of system, specific method includes,
S1, TCASII airborne collision avoidance system power on, and TCASII airborne collision avoidance system receives and dispatches host reading platform flight performance parameter
Inquiry table, and if so, the flight performance parameter inquiry table information of aircraft platform is saved and record, into S2；Otherwise, enter
S6；
S2 obtains aircraft platform flight performance parameter, and judges whether to obtain successfully, if obtained successfully, carries out S3；If obtained
Take it is unsuccessful, carry out repeat acquisition, repeat times of acquisition reach repetition times of acquisition threshold value, then report parameter obtain failure；
S3 detects aircraft platform flight performance parameter, if all normal, into S4, corresponding aircraft platform is otherwise reported to fly
Row performance parameter failure, into S2；
S4 carries out classification processing to aircraft platform flight performance parameter, into S5；
S5, start-up parameter table look-up module, to treated, aircraft platform flight performance parameter is tabled look-up, and it is airborne to obtain TCASII
The related flying quality limitation input parameter that anti-collision system core algorithm needs, and give the parameter to TCASII airborne collision avoidance system
Core algorithm of uniting is handled；Return to S2；
The platform flying quality limitation of S6, TCASII airborne collision avoidance system automatically processes subsystem and uses the aircraft defaulted in software
The flight performance parameter inquiry table of platform, and the flight performance parameter inquiry table of aircraft platform is automatically generated in FLASH, as
Power on use next time.
3. processing method according to claim 2, the method also includes in continuous N number of period S3 if detected winged
Machine platform flight performance parameter failure is limited defeated using the aeroplane performance that TCASII airborne collision avoidance system tail portion discrete lines provide
Enter；Wherein, N is the natural number more than or equal to 2.
4. processing method according to claim 2, the method also includes if continuous N periodic report parameter obtains
Failure then limits input using the aeroplane performance that TCASII airborne collision avoidance system tail portion discrete lines provide；Wherein, M be greater than etc.
In 1 natural number.
5. processing method according to claim 3 or 4, the method also includes when use TCASII airborne collision avoidance system
When the aeroplane performance limitation input that tail portion discrete lines provide is also unavailable, aircraft platform flying quality is set without limitation.
6. processing method according to claim 3, the N is equal to 3.
7. processing method according to claim 4, the M is equal to 3.
8. the method for processing method according to claim 2, parameter query includes, the platform flight performance parameter is looked into
Inquiry table is solidificated in airborne collision avoidance processing software for inquiring.
9. the method for processing method according to claim 2, parameter query includes, the platform flight performance parameter is looked into
Inquiry table is solidificated in the FLASH of the processing module where the anticollision core algorithm of TCASII airborne collision avoidance system in the form of configuration file
In for inquiring.
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