CN108922309A - A kind of aircraft magnetic deviation calibrated analog training system - Google Patents
A kind of aircraft magnetic deviation calibrated analog training system Download PDFInfo
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- CN108922309A CN108922309A CN201810920945.3A CN201810920945A CN108922309A CN 108922309 A CN108922309 A CN 108922309A CN 201810920945 A CN201810920945 A CN 201810920945A CN 108922309 A CN108922309 A CN 108922309A
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/24—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer including display or recording of simulated flight path
- G09B9/245—Simulation of compasses, gyroscopes
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/24—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer including display or recording of simulated flight path
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Abstract
The invention discloses a kind of aircraft magnetic deviation calibrated analog training systems, belong to plane simulation training equipment technical field, it includes normal orientation instrument, model aircraft, servomechanism and display and operation platform, the normal orientation instrument is set to the servomechanism side, for providing magnetic north direction for the model aircraft, the normal orientation instrument includes electronic compass, fixture and bracket, the electronic compass is arranged on the bracket by the fixture, the electronic compass and the display and operation platform transmit information, the model aircraft is arranged in the servomechanism, the model aircraft is equipped with magnetic course transmitter, the magnetic course transmitter and the servomechanism transmit information, the servomechanism and the display and operation platform transmit information.Aircraft magnetic deviation calibrated analog training system of the invention, for the training of aircraft magnetic deviation calibrated analog, using intuitive and convenient, training function is more, and training effect is good.
Description
Technical field
The present invention relates to plane simulation training equipment technical field, specifically a kind of aircraft magnetic deviation calibrated analog training systems
System.
Background technique
Mariner's compass can be all usually installed aboard, these mariner's compasses include magnetic compass, directional gyro, top
Spiral shell compass, gyro-mag, telecompass, Strapdown Attitude Heading Reference System and laser-inertial navigation system etc., are mainly used for provider
Position benchmark, measurement, instruction vector are very high to the exact requirements of mariner's compass, therefore usually need to airborne compass, boat
Appearance system etc. is calibrated；In the calibration training of aircraft magnetic deviation, using actual airplane waste of manpower financial resources, or even aircraft is caused to damage
Condition of the injury condition, therefore, it is necessary to a kind of aircraft magnetic deviation calibrated analog training systems.
The patent that notification number is 104406578 B of CN discloses a kind of aircraft compass course and guides and compass guidance calibration
System and method, the system include microprocessor, magnetic course transmitter, main display terminal, follow display terminal and input equipment；
The inside of microprocessor is equipped with 8 calibration process modules or 12 calibration process modules；Magnetic course transmitter is located at aircraft bottom
Or on the aircraft longitudinal axis line at top or it is parallel to the position of aircraft longitudinal axis line, and its course is consistent with the course of aircraft；Main display
Terminal is arranged in the aircraft cockpit for facilitating flight crew to check；It follows terminal on tractor, is driven for instructing
Accurate towing aircraft and stopping a train at a target point when the person's of sailing swing a compass；It can instruct traction driver and cockpit compass calibration people simultaneously in this way
The function of member's carry out compass calibration, prover time is short, high-efficient, and labor intensity is low, and the compass for being suitable for various aircrafts is calibrated,
To compass testing platform require low, manufacturing cost is low, structure is simple, high in technological content, and the market demand is big, has a extensive future, still,
The invention cannot be used for the training of aircraft magnetic deviation calibrated analog.Notification number is that the patent of CN100568317 discloses one kind for flying
The simulated training system control device of machine comprehensive coverage professional technician training is related to protecting what ground used with airplane synthetic
Hinder related device.The device is made of analog capsule cabin, main control computer and its interface system, monitoring Demonstration table etc., comprehensive fortune
With Virtual instrument dash board control technology, single machine multi-touch screen control technology, utilizes a display to substitution part installing equipment and complete
Flight Instrument template die is quasi-, and the control for carrying out three-dimensional artificial instrument over the display show, using single machine multi-touch screen with it is more
Platform LCD display control technology realizes the multiple touch screens of a main control computer drive control and Duo Tai LCD display, can be into
The training of row aircraft various states work simulation, the training of detection device operation simulation, troubleshooting technical ability and department enclosure dismount simulated training
It is demonstrated with multimedia software, realizes that airplane synthetic guarantee is multi-specialized, multidisciplinary training, and cost performance is high, maintainability is good, can rise
Grade ability is strong, and still, which cannot be used for simulation aircraft magnetic deviation calibration training.
Summary of the invention
In view of this, in view of the deficiencies of the prior art, the present invention provides one kind for simulate aircraft magnetic deviation calibration training
Aircraft magnetic deviation calibrated analog training system.
In order to solve the above technical problems, the technical solution adopted by the present invention is that：A kind of aircraft magnetic deviation calibrated analog training
System, it is characterised in that：Including normal orientation instrument, model aircraft, servomechanism and display and operation platform, the normal orientation instrument is set
It is placed in the servomechanism side, for providing magnetic north direction for the model aircraft, the normal orientation instrument includes electronics sieve
The electronic compass and the display on the bracket is arranged by the fixture in disk, fixture and bracket, the electronic compass
Operation bench transmits information, and the model aircraft is arranged in the servomechanism, and the model aircraft is sensed equipped with magnetic heading
Device, the magnetic course transmitter and the servomechanism transmit information, and the servomechanism and display and operation platform transmission are believed
Breath.
Preferably, the servomechanism includes servomechanism platform, servomechanism driving assembly and the control servomechanism
The servomechanism controller of driving assembly, the servomechanism platform includes cylinder table, and scale is arranged in the cylinder table top edge
Disk, the cylinder table are equipped with rotating circular disk, and the rotating circular disk is driven by the servomechanism being arranged in the cylinder table
Dynamic Component driver, the rotating circular disk are equipped with protective fence, are arranged on the rotating circular disk multiple for fixing the aircraft mould
The wheel wheel shelves of type.
Preferably, the servomechanism driving assembly includes stepper motor, shaft coupling and planetary gear, under the rotating circular disk
The driven wheel of the planetary gear is fixedly installed, the driving wheel of the planetary gear connects driving shaft, and the driving shaft passes through described
Axis device is connect with the motor.
Preferably, the servomechanism controller includes that DC power supply, controllor for step-by-step motor and navigation attitude control box, described
DC power supply is that the controllor for step-by-step motor and the navigation attitude control box power supply, the controllor for step-by-step motor and the stepping
Motor is connected by signal wire, and the magnetic course transmitter and navigation attitude control box transmit information, the step motor control
Device and navigation attitude control box transmit information with the display and operation platform.
Preferably, the display and operation platform includes stage body, AC power source, host computer, main display, synthesis display screen,
The AC power source is the host computer, the main display and synthesis display screen power supply, the main display, described
Synthesis display screen and navigation attitude control box are connect with the host computer, and the synthesis display screen shows the electronic compass
Box information is controlled with the navigation attitude.
Preferably, the model aircraft includes head, body, wing, empennage, undercarriage and hanger, the head, machine
It is detachably assembled between body, wing, empennage, undercarriage and hanger.
Preferably, the model aircraft material is aluminium alloy.
A kind of analogy method of aircraft magnetic deviation calibrated analog training system, includes the following steps：1）Far from electronic equipment
Region is found out using the normal orientation instrument works as magnetic north, and the model aircraft is moved to 0 degree of position of magnetic heading；
2）Power on, navigation attitude is controlled into " DG-MAG " switch on box and is placed in the position " MAG "；In the case where preparing picture, continuously press
Twice, control panel enters magnetic deviation calibration menu screen to " menu " key, shows " MAGCAL START ", presses the navigation attitude control box
On " confirmation " key after magnetic deviation calibration start, control panel shows " TURN TOXXX ", and calibration process starts；
3）The current course of the model aircraft is measured using the normal orientation instrument, and the model aircraft is gone to 0 °, is stopped
The only model aircraft rotation adjusts navigation attitude control box to 45 °, presses " confirmation " key；
4）It adjusts navigation attitude and controls box, the model aircraft is made successively to go to 45 °, 90 °, 135 °, 180 °, 225 °, 270 °, 315 °,
Magnetic deviation calibration finishes；
5）Using the host computer and main display of the display and operation platform, calculate magnetic heading error, draw compass calibration table and
Compass diviation compensation curve.
Compared with prior art, beneficial effects of the present invention are as follows：
Aircraft magnetic deviation calibrated analog training system of the invention can be used for completing normal orientation instrument training, calibration compass method step
Rapid training, magnetic heading error calculate, compass calibration table fill in compass diviation compensation Drawing of Curve, vdiverse in function, training is intuitive, complete
Face；The normal orientation instrument is arranged in the servomechanism side, for the measurement in earth's magnetic field, can both be indicated by mechanical indicator
It sails to and course electronic data can be exported, the display and operation platform receives course electronic data, and course information is shown
On synthesis display screen, while user of service can be used computer housing and calculate magnetic heading error according to course electronic data；It is described
Model aircraft is designed manufacture in such a way that skeleton adds covering, and head, wing, empennage, undercarriage and hanger are disassembled,
Facilitate carrying and installation, model aircraft uses aluminum alloy material, light quality and stability is good；Quarter on the servomechanism platform
Scale facilitates model aircraft to be adjusted the angle according to normal orientation instrument, and the wheel wheel shelves on servomechanism platform are used for fastening aircraft,
Prevent servomechanism platform in rotation, model aircraft occurs to break away or movement, rotating circular disk are equipped with protective fence, can not only protect
Protect model aircraft, and convenient rotation rotating circular disk manually；It is aobvious to provide data for interaction platform of the display and operation platform as user
Show, the function of manipulation of switches, the magnetic heading information of electronic compass can be shown on synthesis display screen, and electricity can be passed through
Brain server controls the operating of servomechanism driving assembly, integrates observation, regulation, and when use is more convenient；Navigation attitude controls box
The main component for calibrating electronic compass error carries out system using navigation attitude control box by the mobile vector of multiple multi-angle
The training of magnetic deviation calibrated analog is realized in correction.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of servomechanism in the present invention；
Fig. 2 is the structural schematic diagram of Plays azimuth device of the present invention；
Fig. 3 is the structural schematic diagram of servomechanism platform in the present invention；
Fig. 4 is circuit diagram of the invention；
Fig. 5 is that compass calibration indicates example in the embodiment of the present invention four：
Fig. 6 is the compass diviation compensation curve graph of 4 simulated experiments in Fig. 5；
Wherein, 1- electronic compass, 2- fixture, 3- bracket, 4- model aircraft, 5- magnetic course transmitter, 6- servomechanism controller,
7- cylinder table, 8- dial, 9- rotating circular disk, 10- protective fence, 11- wheel wheel shelves, 12- stepper motor, 13- shaft coupling, 14-
Planetary gear.
Specific embodiment
For a better understanding of the present invention, the contents of the present invention, but this hair are further fairly set out below with reference to embodiment
Bright protection content is not limited solely to the following examples.In the following description, give a large amount of concrete details so as to
More thorough understanding of the invention is provided.It will be apparent, however, to one skilled in the art that the present invention can be with
It is carried out without one or more of these details.
Embodiment one
As shown in Fig. 1 ~ 4, a kind of aircraft magnetic deviation calibrated analog training system, including normal orientation instrument, model aircraft, servomechanism
With display and operation platform, the normal orientation instrument is set to the servomechanism side, for providing magnetic north for the model aircraft
Direction, the normal orientation instrument include electronic compass 1, fixture 2 and bracket 3, and the electronic compass 1 is arranged by the fixture 2
On the bracket 3, the electronic compass 1 and the display and operation platform transmit information, the setting of model aircraft 4 it is described with
In dynamic system, the model aircraft 4 is equipped with magnetic course transmitter 5, and the magnetic course transmitter 5 is transmitted with the servomechanism
Information, the servomechanism and the display and operation platform transmit information.
The servomechanism includes servomechanism platform, servomechanism driving assembly and the control servomechanism driving assembly
Servomechanism controller 6, the servomechanism platform includes cylinder table 7, and dial 8, institute is arranged in 7 top edge of cylinder table
Cylinder table 7 is stated equipped with rotating circular disk 9, the rotating circular disk 9 is driven by the servomechanism being arranged in the cylinder table 7
Component driver, the rotating circular disk 9 are equipped with protective fence 10, and setting three are used to fix the aircraft on the rotating circular disk 9
The wheel wheel shelves 11 of model 4.
The aircraft magnetic deviation calibrated analog training system of the embodiment of the present invention can be used for completing normal orientation instrument training, calibration
The training of compass method and step, magnetic heading error calculate, compass calibration table is filled in and compass diviation compensation Drawing of Curve, vdiverse in function, instruction
Practice intuitive, comprehensive；The normal orientation instrument is arranged in the servomechanism side, for the measurement in earth's magnetic field, can both pass through machine
Tool pointer indicates course, and can export course electronic data, and the display and operation platform receives course electronic data, and by course
Information is shown on synthesis display screen, while user of service can be used computer housing and calculate magnetic heading according to course electronic data
Error；
In addition, the dial on the servomechanism platform, facilitates model aircraft to be adjusted the angle according to normal orientation instrument, servomechanism
Wheel wheel shelves on platform are used for fastening aircraft, prevent servomechanism platform in rotation, and sideslip or mobile, rotation occur for model aircraft
Turn disk equipped with protective fence, model aircraft, and convenient rotation rotating circular disk manually can not only be protected.
Embodiment two
As shown in Fig. 1 ~ 4, a kind of aircraft magnetic deviation calibrated analog training system, including normal orientation instrument, model aircraft, servomechanism
With display and operation platform, the normal orientation instrument is set to the servomechanism side, for providing magnetic north for the model aircraft
Direction, the normal orientation instrument include electronic compass 1, fixture 2 and bracket 3, and the electronic compass 1 is arranged by the fixture 2
On the bracket 3, the electronic compass 1 and the display and operation platform transmit information, the setting of model aircraft 4 it is described with
In dynamic system, the model aircraft 4 is equipped with magnetic course transmitter 5, and the magnetic course transmitter 5 is transmitted with the servomechanism
Information, the servomechanism and the display and operation platform transmit information.
The servomechanism includes servomechanism platform, servomechanism driving assembly and the control servomechanism driving assembly
Servomechanism controller 6, the servomechanism platform includes cylinder table 7, and dial 8, institute is arranged in 7 top edge of cylinder table
Cylinder table 7 is stated equipped with rotating circular disk 9, the rotating circular disk 9 is driven by the servomechanism being arranged in the cylinder table 7
Component driver, the rotating circular disk 9 are equipped with protective fence 10, and setting three are used to fix the aircraft on the rotating circular disk 9
The wheel wheel shelves 11 of model 4.
The aircraft magnetic deviation calibrated analog training system of the embodiment of the present invention, with embodiment one the difference is that：It is described
Servomechanism driving assembly includes stepper motor 12, shaft coupling 13 and planetary gear 14, under the rotating circular disk 9 described in fixed setting
The driven wheel of planetary gear, the driving wheel of the planetary gear connect driving shaft, the driving shaft by the shaft coupling 13 with it is described
Stepper motor 12 connects；
The servomechanism controller includes that DC power supply, controllor for step-by-step motor and navigation attitude control box, the DC power supply are
The controllor for step-by-step motor and navigation attitude control box power supply, the controllor for step-by-step motor and the stepper motor pass through letter
The connection of number line, the magnetic course transmitter and navigation attitude control box transmit information, the controllor for step-by-step motor and the boat
Attitude control box transmits information with the display and operation platform.
Embodiment three
The aircraft magnetic deviation calibrated analog training system of the embodiment of the present invention, with embodiment one, two the difference is that：It is described aobvious
Show that operation bench includes stage body, AC power source, host computer, main display, synthesis display screen, the AC power source is the computer
Host, the main display and synthesis display screen power supply, the main display, the synthesis display screen and the navigation attitude control
Box processed is connect with the host computer, and the synthesis display screen shows the electronic compass and navigation attitude control box information.
In the embodiment of the present invention, interaction platform of the display and operation platform as user, provide data show, the function of manipulation of switches
Can, the magnetic heading information of electronic compass can be shown on synthesis display screen, and can be controlled by host computer servo-actuated
The operating of system drive component integrates observation, regulation, and when use is more convenient；Navigation attitude control box is that calibration electronic compass misses
The main component of difference carries out system compensation using navigation attitude control box, realizes magnetic deviation school by the mobile vector of multiple multi-angle
Quasi- simulated training.
Example IV
As shown in Fig. 1 ~ 6, a kind of aircraft magnetic deviation calibrated analog training system, including normal orientation instrument, model aircraft, servomechanism
With display and operation platform, the normal orientation instrument is set to the servomechanism side, for providing magnetic north for the model aircraft
Direction, the normal orientation instrument include electronic compass 1, fixture 2 and bracket 3, and the electronic compass 1 is arranged by the fixture 2
On the bracket 3, the electronic compass 1 and the display and operation platform transmit information, the setting of model aircraft 4 it is described with
In dynamic system, the model aircraft 4 is equipped with magnetic course transmitter 5, and the magnetic course transmitter 5 is transmitted with the servomechanism
Information, the servomechanism and the display and operation platform transmit information.
The servomechanism includes servomechanism platform, servomechanism driving assembly and the control servomechanism driving assembly
Servomechanism controller 6, the servomechanism platform includes cylinder table 7, and dial 8, institute is arranged in 7 top edge of cylinder table
Cylinder table 7 is stated equipped with rotating circular disk 9, the rotating circular disk 9 is driven by the servomechanism being arranged in the cylinder table 7
Component driver, the rotating circular disk 9 are equipped with protective fence 10, and setting three are used to fix the aircraft on the rotating circular disk 9
The wheel wheel shelves 11 of model 4.
The servomechanism driving assembly includes stepper motor 12, shaft coupling 13 and planetary gear 14, under the rotating circular disk 9
The driven wheel of the planetary gear is fixedly installed, the driving wheel of the planetary gear connects driving shaft, and the driving shaft passes through described
Axis device 13 is connect with the stepper motor 12；
The servomechanism controller includes that DC power supply, controllor for step-by-step motor and navigation attitude control box, the DC power supply are
The controllor for step-by-step motor and navigation attitude control box power supply, the controllor for step-by-step motor and the stepper motor pass through letter
The connection of number line, the magnetic course transmitter and navigation attitude control box transmit information, the controllor for step-by-step motor and the boat
Attitude control box transmits information with the display and operation platform；
The display and operation platform includes stage body, AC power source, host computer, main display, synthesis display screen, the AC power source
For the host computer, the main display and the synthesis display screen power supply, the main display, the synthesis display screen and
The navigation attitude control box is connect with the host computer, and the synthesis display screen shows the electronic compass and the navigation attitude control
Box information processed；
The aircraft magnetic deviation calibrated analog training system of the embodiment of the present invention, with embodiment one, two, three the difference is that：Institute
Stating model aircraft 4 includes head, body, wing, empennage, undercarriage and hanger, and the head, wing, empennage, rises and falls at body
It is detachably assembled between frame and hanger, facilitates carrying and installation, 4 material of model aircraft is aluminium alloy, light quality and heavily fortified point
Gu durable.
The analogy method of the aircraft magnetic deviation calibrated analog training system of the embodiment of the present invention, includes the following steps：1）Remote
It is found out from electronics area using the normal orientation instrument and works as magnetic north, the model aircraft is moved to 0 degree of position of magnetic heading
It sets；
2）Power on, navigation attitude is controlled into " DG-MAG " switch on box and is placed in the position " MAG "；In the case where preparing picture, continuously press
Twice, control panel enters magnetic deviation calibration menu screen to " menu " key, shows " MAGCAL START ", presses the navigation attitude control box
On " confirmation " key after magnetic deviation calibration start, control panel shows " TURN TOXXX ", and calibration process starts；
3）The current course of the model aircraft is measured using the normal orientation instrument, and the model aircraft is gone to 0 °, is stopped
The only model aircraft rotation adjusts navigation attitude control box to 45 °, presses " confirmation " key；
4）It adjusts navigation attitude and controls box, the model aircraft is made successively to go to 45 °, 90 °, 135 °, 180 °, 225 °, 270 °, 315 °,
Magnetic deviation calibration finishes；
5）Using the host computer and main display of the display and operation platform, calculate magnetic heading error, draw compass calibration table and
Compass diviation compensation curve.
As can be seen that the error of each magnetic deviation calibration is no more than ± 5% from Fig. 5 ~ Fig. 6, and with magnetic deviation calibration time
Several increases, compass diviation compensation curve is gradually gentle, and the effect of compass calibration enhances therewith, the aircraft magnetic deviation school of the embodiment of the present invention
The simulated training effect of quasi- simulated training system is good, and student is enabled to carry out good training to the calibration of aircraft magnetic deviation.
Finally, it is stated that the above examples are only used to illustrate the technical scheme of the present invention and are not limiting, this field is common
Other modifications or equivalent replacement that technical staff makes technical solution of the present invention, without departing from technical solution of the present invention
Spirit and scope, be intended to be within the scope of the claims of the invention.
Claims (8)
1. a kind of aircraft magnetic deviation calibrated analog training system, it is characterised in that：Including normal orientation instrument, model aircraft, servo-actuated system
System and display and operation platform, the normal orientation instrument is set to the servomechanism side, for providing magnetic for the model aircraft
The north is to the normal orientation instrument includes electronic compass, fixture and bracket, and the electronic compass is arranged by the fixture in institute
It states on bracket, the electronic compass and the display and operation platform transmit information, and the model aircraft is arranged in the servomechanism
On, the model aircraft is equipped with magnetic course transmitter, and the magnetic course transmitter and the servomechanism transmit information, described
Servomechanism and the display and operation platform transmit information.
2. aircraft magnetic deviation calibrated analog training system as described in claim 1, it is characterised in that：The servomechanism include with
The servomechanism controller of dynamic system bay, servomechanism driving assembly and the control servomechanism driving assembly, it is described servo-actuated
System bay includes cylinder table, and dial is arranged in the cylinder table top edge, and the cylinder table is equipped with rotating circular disk, the rotation
Turn disk to be driven by the servomechanism driving assembly being arranged in the cylinder table, the rotating circular disk is equipped with protection
Column is arranged on the rotating circular disk multiple for fixing the wheel wheel shelves of the model aircraft.
3. aircraft magnetic deviation calibrated analog training system as claimed in claim 2, it is characterised in that：The servomechanism driving group
Part includes stepper motor, shaft coupling and planetary gear, and the driven wheel of the planetary gear, the row are fixedly installed under the rotating circular disk
The driving wheel of star-wheel connects driving shaft, and the driving shaft is connect by the shaft coupling with the motor.
4. aircraft magnetic deviation calibrated analog training system as claimed in claim 3, it is characterised in that：The servomechanism controller
Box is controlled including DC power supply, controllor for step-by-step motor and navigation attitude, the DC power supply is the controllor for step-by-step motor and institute
Navigation attitude control box power supply is stated, the controllor for step-by-step motor is connect with the stepper motor by signal wire, and the magnetic heading passes
Sensor and navigation attitude control box transmit information, and the controllor for step-by-step motor and navigation attitude control box are grasped with the display
It controls platform and transmits information.
5. aircraft magnetic deviation calibrated analog training system as claimed in claim 4, it is characterised in that：The display and operation platform includes
Stage body, AC power source, host computer, main display, synthesis display screen, the AC power source are the host computer, the master
Display screen and synthesis display screen power supply, the main display, the synthesis display screen and navigation attitude control box are and institute
Host computer connection is stated, the synthesis display screen shows the electronic compass and navigation attitude control box information.
6. aircraft magnetic deviation calibrated analog training system as claimed in claim 1 or 5, it is characterised in that：The model aircraft packet
Head, body, wing, empennage, undercarriage and hanger are included, it can between the head, body, wing, empennage, undercarriage and hanger
Disassembly assembling.
7. aircraft magnetic deviation calibrated analog training system as claimed in claim 6, it is characterised in that：The model aircraft material is
Aluminium alloy.
8. the analogy method of aircraft magnetic deviation calibrated analog training system as claimed in claim 7, it is characterised in that：Including following
Step：1）Work as magnetic north finding out far from electronics area using the normal orientation instrument, the model aircraft is moved to
0 degree of position of magnetic heading；
2）Power on, navigation attitude is controlled into " DG-MAG " switch on box and is placed in the position " MAG "；In the case where preparing picture, continuously press
Twice, control panel enters magnetic deviation calibration menu screen to " menu " key, shows " MAGCAL START ", presses the navigation attitude control box
On " confirmation " key after magnetic deviation calibration start, control panel shows " TURN TOXXX ", and calibration process starts；
3）The current course of the model aircraft is measured using the normal orientation instrument, and the model aircraft is gone to 0 °, is stopped
The only model aircraft rotation adjusts navigation attitude control box to 45 °, presses " confirmation " key；
4）It adjusts navigation attitude and controls box, the model aircraft is made successively to go to 45 °, 90 °, 135 °, 180 °, 225 °, 270 °, 315 °,
Magnetic deviation calibration finishes；
5）Using the host computer and main display of the display and operation platform, calculate magnetic heading error, draw compass calibration table and
Compass diviation compensation curve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810920945.3A CN108922309B (en) | 2018-08-14 | 2018-08-14 | Airplane compass calibration simulation training system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810920945.3A CN108922309B (en) | 2018-08-14 | 2018-08-14 | Airplane compass calibration simulation training system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108922309A true CN108922309A (en) | 2018-11-30 |
| CN108922309B CN108922309B (en) | 2024-05-28 |
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Cited By (5)
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|---|---|---|---|---|
| CN109916385A (en) * | 2019-04-11 | 2019-06-21 | 中国民航大学 | A kind of multi-operation mode aircraft standby compass tester |
| CN111060134A (en) * | 2019-12-10 | 2020-04-24 | 中船航海科技有限责任公司 | Device for measuring follow-up error of magnetic heading sending device |
| CN112665611A (en) * | 2020-12-17 | 2021-04-16 | 陕西宝成航空仪表有限责任公司 | Airborne magnetic compass azimuth error calibration device |
| CN113932831A (en) * | 2021-09-24 | 2022-01-14 | 成都飞机工业（集团）有限责任公司 | Aircraft magnetic heading calibration method for laser aiming without reference object |
| CN114023144A (en) * | 2021-11-03 | 2022-02-08 | 中国民航大学 | Aircraft standby compass calibration teaching platform |
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| CN109916385A (en) * | 2019-04-11 | 2019-06-21 | 中国民航大学 | A kind of multi-operation mode aircraft standby compass tester |
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| CN111060134A (en) * | 2019-12-10 | 2020-04-24 | 中船航海科技有限责任公司 | Device for measuring follow-up error of magnetic heading sending device |
| CN112665611A (en) * | 2020-12-17 | 2021-04-16 | 陕西宝成航空仪表有限责任公司 | Airborne magnetic compass azimuth error calibration device |
| CN112665611B (en) * | 2020-12-17 | 2022-10-25 | 陕西宝成航空仪表有限责任公司 | Airborne magnetic compass azimuth error calibration device |
| CN113932831A (en) * | 2021-09-24 | 2022-01-14 | 成都飞机工业（集团）有限责任公司 | Aircraft magnetic heading calibration method for laser aiming without reference object |
| CN113932831B (en) * | 2021-09-24 | 2023-12-08 | 成都飞机工业（集团）有限责任公司 | Aircraft magnetic heading calibration method for laser aiming without reference object |
| CN114023144A (en) * | 2021-11-03 | 2022-02-08 | 中国民航大学 | Aircraft standby compass calibration teaching platform |
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