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CN107817006A - A kind of angle of attack sensor self-sensing method - Google Patents

A kind of angle of attack sensor self-sensing method Download PDF

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Publication number
CN107817006A
CN107817006A CN201711243689.0A CN201711243689A CN107817006A CN 107817006 A CN107817006 A CN 107817006A CN 201711243689 A CN201711243689 A CN 201711243689A CN 107817006 A CN107817006 A CN 107817006A
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China
Prior art keywords
sensor
angle
normal
failure
attack
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CN201711243689.0A
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CN107817006B (en
Inventor
胡延国
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C25/00Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Transmission And Conversion Of Sensor Element Output (AREA)

Abstract

The invention discloses a kind of angle of attack sensor self-sensing method, belong to sensor detecting field.Including:Step 1: whether the acquisition interface of detection controller is normal;If normal, step 2 is carried out;Otherwise, then acquisition interface failure is recorded;Step 2: whether detection sensor output signal is normal with value;If normal, step 3 is carried out;Otherwise, then pair recorded with value failure;Step 3: whether detection sensor is in extreme position output signal and and be worth normal;If normal, step 4 is carried out;No survey, then recorded to sensor output signal failure and with value failure;Step 4: whether detection angle of attack sensor weathercock there is stuck failure;Step 5: fault comprehensive is carried out to angle of attack sensor Autonomous test result;The present invention improves the fault location accuracy of this self-sensing method;Using and value judge with both sides tilt limit position when sensor outgoing position determination methods, improve angle of attack sensor failure checking cover ratio.

Description

A kind of angle of attack sensor self-sensing method
Technical field
The invention belongs to sensor detecting field, and in particular to a kind of angle of attack sensor self-sensing method.
Background technology
Angle of attack sensor has highly important effect to the flight safety of aircraft, the normal operation of flight control system from The normal work of angle of attack sensor is not opened.Some angle of attack sensor weathercocks do not possess long distance deflection, due to using preceding wind direction Change cause sensor output signal to be a random value, therefore using can not be to its output signal before this angle of attack sensor Correctness judged;Only to same mechanical remaining during some angle of attack sensor Autonomous tests.The failure pair of angle of attack sensor The flight safety of aircraft can produce more serious influence.
Therefore, should comprehensively be detected to angle of attack sensor output signal before use, the inspection of angle of attack sensor is improved Look into coverage rate.
The content of the invention
The purpose of the present invention:In order to solve the above problems, the present invention proposes a kind of angle of attack sensor self-sensing method, solution Determine the Autonomous test problem of the angle of attack sensor with long distance deflection, improved angle of attack sensor Autonomous test coverage rate.
Technical scheme:A kind of angle of attack sensor self-sensing method, comprises the following steps:
Step 1: whether the acquisition interface of detection controller is normal;
Carry out positive definite value excitation and the excitation of reverse definite value respectively to the acquisition interface of controller by excitation wires, check Whether acquisition interface is normal;
If normal, step 2 is carried out;
Otherwise, then acquisition interface failure is recorded;
Step 2: whether detection sensor output signal is normal with value;
Collection sensor exports high-end centering and takes out terminal voltage UH-CTAnd terminal voltage U is taken out in sensor output low side centeringL-CT, two Person be added and threshold voltage USUM, by judging USUMJudge whether sensor output is normal;
If normal, step 3 is carried out;
Otherwise, then discovery is recorded with value failure;
Step 3: whether detection sensor is in extreme position output signal and and be worth normal;
Realize that weathercock forwards/reverse deflects by long distance deflection, after deflecting into extreme position, collection sensor output Whether signal is normal;
If normal, step 4 is carried out;
No survey, then the sensor output signal failure to discovery and and value failure record;
Step 4: whether detection angle of attack sensor weathercock there is stuck failure;
Controller control angle of attack sensor carries out the positive deflection of short time or reversely deflection, sensor weathercock is not stopped The extreme position of both sides is stayed in, whether controller gathers angle of attack sensor output signal also in extreme position;
If showing the stuck failure of angle of attack sensor weathercock occur in the extreme position,
Show angle of attack sensor weathercock normal work if the extreme position is not at;
Step 5: fault comprehensive is carried out to angle of attack sensor Autonomous test result;
Acquisition interface fault comprehensive is controller failure, and the fault comprehensive occurred in remaining detection process is angle of attack sensor Failure.
Preferably, the controller in the step 1 is provided with for carrying out positive definite value excitation or the excitation of reverse energization Circuit;
The excitation wires are connected by the analogue collection module of acquisition interface and controller.
Preferably, the acquisition interface is provided with relay;
Switching between excitation wires and external sensor signal output circuit is completed by the relay.
Technical solution of the present invention advantageous effects:A kind of angle of attack sensor self-sensing method of the present invention solves purely mechanic Formula uses preceding Autonomous test problem without long distance deflection weather vane type angle of attack sensor, before angle of attack sensor output signal is detected, Detect controller acquisition interface in itself whether normal work, improve the fault location accuracy of this self-sensing method;Using with Value judgement and sensor outgoing position determination methods during the tilt limit position of both sides, improve angle of attack sensor fault detect covering Rate.
Brief description of the drawings
Fig. 1 is that the controller of a preferred embodiment of angle of attack self-sensing method of the present invention shows with angle of attack sensor annexation It is intended to;
Fig. 2 is the detection method schematic flow sheet of a preferred embodiment of angle of attack self-sensing method of the present invention.
Embodiment
To make the purpose, technical scheme and advantage that the present invention is implemented clearer, below in conjunction with the embodiment of the present invention Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or class As label represent same or similar element or the element with same or like function.Described embodiment is the present invention Part of the embodiment, rather than whole embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to uses It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people The every other embodiment that member is obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.Under Embodiments of the invention are described in detail with reference to accompanying drawing for face.
As shown in Figure 1 to Figure 2:The present invention proposes a kind of angle of attack sensor self-sensing method, comprises the following steps:
Step a, whether normal acquisition interface is detected:
Controller will switch and 1. push excitation wires position;
Controller will switch and 2. push " forward direction " position, output positive incentive signal is carried out constant value to acquisition interface and swashs Encourage;
Collection value is checked after Acquisition Circuit whether in the range of desired excitation constant value, if not in threshold range Failure is recorded and declares acquisition interface failure, thinks that acquisition interface is normal if in threshold range;
Controller will switch and 2. push " reverse " position, output reverse energization signal is carried out constant value to acquisition interface and swashs Encourage;
Collection value is checked after Acquisition Circuit whether in the range of desired excitation constant value, if not in threshold range Failure is recorded and declares acquisition interface failure, thinks that acquisition interface is normal if in threshold range;
1. Fig. 1 switches are returned into sensor output signal collection position.
Step b, detection sensor output signal and value it is whether normal:
The H ends of sensor output signal are gathered to CT terminal voltages UH-CT
The L ends of sensor output signal are gathered to CT terminal voltages UL-CT,
By UH-CTWith UL-CTBe added and threshold voltage USUM, check USUMWhether in desired and value threshold range, if do not existed Then failure is recorded in threshold range and declares sensor and value failure, angle of attack sensor is thought if in threshold range It is normal with value.
Step c, whether detection sensor output signal in certain side pole extreme position is normal:
Controller control angle of attack sensor weathercock carries out positive long distance and deflects into extreme position;
Controller gathers angle of attack sensor output signal and its with value whether in desired extreme position threshold range, such as Then failure is recorded not in threshold range and declares sensor signal failure, thinks that the angle of attack passes if in threshold range Sensor signal is normal;
Controller control angle of attack sensor weathercock carries out reverse long distance and deflects into extreme position;
Controller gathers angle of attack sensor output signal and its with value whether in desired extreme position threshold range, such as Then failure is recorded not in threshold range and declares sensor signal failure, thinks that the angle of attack passes if in threshold range Sensor signal is normal.
To prevent that it is stuck in extreme position fault mode, after above-mentioned detecting step is completed, controller control that weathercock from occurring Angle of attack sensor carries out the positive deflection of short time, sensor weathercock is not rested on the extreme position of both sides.
Whether controller gathers angle of attack sensor output signal also in reverse limit position, if being in the extreme position table It is bright the stuck failure of angle of attack sensor weathercock occur, show angle of attack sensor weathercock normal work if the extreme position is not at.
Step d, fault comprehensive is carried out to angle of attack sensor Autonomous test result:
The fault comprehensive occurred in step a detection process is controller acquisition interface failure;
Step b, the fault comprehensive occurred in c detection process is angle of attack sensor failure.
It is last it is to be noted that:The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations.To the greatest extent The present invention is described in detail with reference to the foregoing embodiments for pipe, it will be understood by those within the art that:It is still Technical scheme described in foregoing embodiments can be modified, or which part technical characteristic is equally replaced Change;And these modifications or replacement, the essence of appropriate technical solution is departed from the essence of various embodiments of the present invention technical scheme God and scope.

Claims (3)

  1. A kind of 1. angle of attack sensor self-sensing method, it is characterised in that:Comprise the following steps:
    Step 1: whether the acquisition interface of detection controller is normal;
    Carry out positive definite value excitation and the excitation of reverse definite value respectively to the acquisition interface of controller by excitation wires, check collection Whether interface is normal;
    If normal, step 2 is carried out;
    Otherwise, then acquisition interface failure is recorded;
    Step 2: whether detection sensor output signal is normal with value;
    Collection sensor exports high-end centering and takes out terminal voltage UH-CTAnd terminal voltage U is taken out in sensor output low side centeringL-CT, the two phase Add and threshold voltage USUM, by judging USUMJudge whether sensor output is normal;
    If normal, step 3 is carried out;
    Otherwise, then discovery is recorded with value failure;
    Step 3: whether detection sensor is in extreme position output signal and and be worth normal;
    Realize that weathercock forwards/reverse deflects by long distance deflection, after deflecting into extreme position, gather sensor output signal It is whether normal;
    If normal, step 4 is carried out;
    No survey, then the sensor output signal failure to discovery and and value failure record;
    Step 4: whether detection angle of attack sensor weathercock there is stuck failure;
    Controller control angle of attack sensor carries out the positive deflection of short time or reversely deflection, sensor weathercock is not rested on Whether the extreme position of both sides, controller gather angle of attack sensor output signal also in extreme position;
    If showing the stuck failure of angle of attack sensor weathercock occur in the extreme position,
    Show angle of attack sensor weathercock normal work if the extreme position is not at;
    Step 5: fault comprehensive is carried out to angle of attack sensor Autonomous test result;
    Acquisition interface fault comprehensive is controller failure, and the fault comprehensive occurred in remaining detection process is angle of attack sensor event Barrier.
  2. 2. angle of attack sensor self-sensing method according to claim 1, it is characterised in that:Controller in the step 1 It is provided with the excitation wires for carrying out positive definite value excitation or reverse energization;
    The excitation wires are connected by the analogue collection module of acquisition interface and controller.
  3. 3. angle of attack sensor self-sensing method according to claim 2, it is characterised in that:The acquisition interface be provided with after Electrical equipment;
    Switching between excitation wires and external sensor signal output circuit is completed by the relay.
CN201711243689.0A 2017-11-30 2017-11-30 Self-detection method of attack angle sensor Active CN107817006B (en)

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Application Number Priority Date Filing Date Title
CN201711243689.0A CN107817006B (en) 2017-11-30 2017-11-30 Self-detection method of attack angle sensor

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Application Number Priority Date Filing Date Title
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115038974A (en) * 2020-01-30 2022-09-09 泰雷兹公司 Self-test method for an angle of attack probe, method for checking the air flow rate provided by a group of associated pitot tube probes, angle of attack probe

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2341775C1 (en) * 2007-06-15 2008-12-20 Открытое акционерное общество "ОКБ Сухого" Method of determining aircraft aerodynamic angle
CN103323624A (en) * 2012-03-21 2013-09-25 空中客车运营简化股份公司 Method and device for verifying the consistency of the measurements of the angle-of-attack probe of an aircraft
CN104931007A (en) * 2014-03-18 2015-09-23 空中客车运营简化股份公司 Method and device for automatically estimating parameters linked to the flight of an aircraft
CN104986355A (en) * 2015-07-14 2015-10-21 中航飞机股份有限公司西安飞机分公司 Giving method and giving device of aircraft incidence angle
CN105973180A (en) * 2016-05-13 2016-09-28 中国航空工业集团公司西安飞机设计研究所 AOA (attack of angle) sensor installation zero position verifying method
WO2016164624A1 (en) * 2015-04-07 2016-10-13 Aspen Avionics, Inc. System and method for angle of attack indication with no dedicated sensors and aircraft information
CN106197479A (en) * 2016-08-12 2016-12-07 河南省计量科学研究院 A kind of portable incidence vane calibrating installation
CN106597977A (en) * 2016-12-02 2017-04-26 武汉航空仪表有限责任公司 Circuit for measuring output signal of attack angle sensor

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2341775C1 (en) * 2007-06-15 2008-12-20 Открытое акционерное общество "ОКБ Сухого" Method of determining aircraft aerodynamic angle
CN103323624A (en) * 2012-03-21 2013-09-25 空中客车运营简化股份公司 Method and device for verifying the consistency of the measurements of the angle-of-attack probe of an aircraft
CN104931007A (en) * 2014-03-18 2015-09-23 空中客车运营简化股份公司 Method and device for automatically estimating parameters linked to the flight of an aircraft
WO2016164624A1 (en) * 2015-04-07 2016-10-13 Aspen Avionics, Inc. System and method for angle of attack indication with no dedicated sensors and aircraft information
CN104986355A (en) * 2015-07-14 2015-10-21 中航飞机股份有限公司西安飞机分公司 Giving method and giving device of aircraft incidence angle
CN105973180A (en) * 2016-05-13 2016-09-28 中国航空工业集团公司西安飞机设计研究所 AOA (attack of angle) sensor installation zero position verifying method
CN106197479A (en) * 2016-08-12 2016-12-07 河南省计量科学研究院 A kind of portable incidence vane calibrating installation
CN106597977A (en) * 2016-12-02 2017-04-26 武汉航空仪表有限责任公司 Circuit for measuring output signal of attack angle sensor

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
彭志专等: "飞机攻角侧滑角传感器检测系统", 《传感器技术》 *
钱林奎: "基于PIC16F877的飞机迎、侧角自动检测系统", 《电子机械工程》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115038974A (en) * 2020-01-30 2022-09-09 泰雷兹公司 Self-test method for an angle of attack probe, method for checking the air flow rate provided by a group of associated pitot tube probes, angle of attack probe

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