CN106525032A - Chinese information display method for inertial navigation system - Google Patents

Chinese information display method for inertial navigation system Download PDF

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Publication number
CN106525032A
CN106525032A CN201510575786.4A CN201510575786A CN106525032A CN 106525032 A CN106525032 A CN 106525032A CN 201510575786 A CN201510575786 A CN 201510575786A CN 106525032 A CN106525032 A CN 106525032A
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CN
China
Prior art keywords
information
chinese
data
navigation system
inertial navigation
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Pending
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CN201510575786.4A
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Chinese (zh)
Inventor
马望福
杨黎
张向虎
张玉博
鹿雪玲
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No 618 Research Institute of China Aviation Industry
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No 618 Research Institute of China Aviation Industry
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Application filed by No 618 Research Institute of China Aviation Industry filed Critical No 618 Research Institute of China Aviation Industry
Priority to CN201510575786.4A priority Critical patent/CN106525032A/en
Publication of CN106525032A publication Critical patent/CN106525032A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)

Abstract

The invention belongs to the field of Chinese information processing technology in an inertial navigation system, and specifically relates to a Chinese information display method for an inertial navigation system. According to the Chinese information display method, when Chinese information is stored in an inertial navigation system, the Chinese information in way point data information is stored in a zone bit code mode according to the structure of the way point database; by establishing a Chinese information universal standard transport protocol, the navigation parts and display parts can communicate through Chinese information; by analyzing the Chinese information universal standard transport protocol, the Chinese character dot matrix library can be projected, and the information is displayed on the screen. The method solves the problem that Chinese information cannot be processed in an inertial navigation system, improves the display performance of an inertial navigation system, and enhances the convenience of operation for users.

Description

A kind of Chinese information display methods for inertial navigation system
Technical field
The invention belongs to inertial navigation system information display technology, and in particular to a kind of Chinese information for inertial navigation system shows Show method.
Background technology
Traditional inertial navigation system using navigation information be all navigation data parameters, by the prompting of display data on the screen information Picture, reaches the effect of display.Do not store inside inertial navigation system, do not use Chinese information, system also not to process Chinese letter Breath.This use for allowing for inertial navigation system receives many restrictions, the such as necessary Chinese information in the point data base of air route, Cannot normally use, can only be substituted using completing information processing with numeral or alphabetical form, this use to user causes very big Burden, reduce the quality of navigation product.
The content of the invention
The purpose of the present invention is:A kind of Chinese information display methods for inertial navigation system is proposed, i.e. one kind effectively can be solved Certainly inertial navigation system realizes the processing method of Chinese information application.
The technical scheme that the present invention takes is:
A kind of Chinese information display methods for inertial navigation system, described inertial navigation system include navigation component and control Display unit, be stored with navigation component air route point data base, and each the way point information in the point data base of air route includes the boat The region-position code of waypoint, longitude, latitude and height, the region-position code that is stored with control display unit dot array data storehouse, wherein often Dot matrix of the individual region-position code to the Chinese geographic name that should have the position representation, it is characterised in that the method is comprised the following steps: Navigation component judges that to the navigation information for gathering such as the information is coincide with certain way point information, then by the way point information Packet be sent to control display unit, after control display unit receives way point information, by region-position code information analysis out, And the corresponding dot matrix of the region-position code is obtained according to region-position code dot array data storehouse, and the dot array data is sent to into display device is shown Show.
Especially, the packet of the way point information is sent to control display unit by HB6096 buses by navigation component, and logical Cross the Chinese information universal standard communication protocol set up to be communicated, the Chinese information universal standard communication protocol is based on HB6096 Bus protocol, state matrix and parity check bit are consistent with which, and wherein, each packet has 4 32 data, the Most least-significant byte index value in one 32 data is that 0X77 representative informations are Chinese character 1, minimum 8 in second 32 data It is Chinese character 2 that position index value is 0X78 representative informations, and the most least-significant byte index value in the 3rd 32 data is that 0X79 represents letter Cease for Chinese character 3, it is Chinese character 4 that the most least-significant byte index value in the 4th 32 data is 0X78 representative informations;Each 32 digit High 16 according in are used for transmitting Hanzi section-position code, and most most-significant byte is with binary-coded decimal format transmission area code, secondary most-significant byte with binary-coded decimal Format transmission bit code;The 16th data in each 32 data represent the validity of Hanzi section-position code, 1 effectively, 0 invalid.
The present invention has the advantage that and beneficial effect:The present invention solves the application problem in inertial navigation system to Chinese information, The display capabilities of navigation information are improved, the convenience of user's manipulation is increased.Establish the transmission of HB6096 buses Chinese information Universal standard communication protocol, realize the reasonable layering of system architecture, reached integral transplanting of the Chinese language processing software across model, Improve development efficiency.
Description of the drawings
Fig. 1 is a kind of method general frame figure for inertial navigation system Chinese information processing of the present invention;
Fig. 2 is way point database store structure figure;
Fig. 3 is Chinese information transmission universal standard communications protocol format chart.
Specific embodiment
Below so that inertial navigation system is processed to air route point data base Air China waypoint Chinese as an example, with reference to accompanying drawing, to a kind of use It is introduced in the method for inertial navigation system Chinese information processing, general frame is shown in Fig. 1, comprises the following steps that:
A kind of Chinese information display methods for inertial navigation system, described inertial navigation system include navigation component and control Display unit, be stored with navigation component air route point data base, and each the way point information in the point data base of air route includes the boat The region-position code of waypoint, longitude, latitude and height, the region-position code that is stored with control display unit dot array data storehouse, wherein often Dot matrix of the individual region-position code to the Chinese geographic name that should have the position representation, it is characterised in that the method is comprised the following steps: Navigation component judges that to the navigation information for gathering such as the information is coincide with certain way point information, then by the way point information Packet be sent to control display unit, after control display unit receives way point information, by region-position code information analysis out, And the corresponding dot matrix of the region-position code is obtained according to region-position code dot array data storehouse, and the dot array data is sent to into display device is shown Show.
Especially, the packet of the way point information is sent to control display unit by HB6096 buses by navigation component, and logical Cross the Chinese information universal standard communication protocol set up to be communicated, the Chinese information universal standard communication protocol is based on HB6096 Bus protocol, state matrix and parity check bit are consistent with which, and wherein, each packet has 4 32 data, the Most least-significant byte index value in one 32 data is that 0X77 representative informations are Chinese character 1, minimum 8 in second 32 data It is Chinese character 2 that position index value is 0X78 representative informations, and the most least-significant byte index value in the 3rd 32 data is that 0X79 represents letter Cease for Chinese character 3, it is Chinese character 4 that the most least-significant byte index value in the 4th 32 data is 0X78 representative informations;Each 32 digit High 16 according in are used for transmitting Hanzi section-position code, and most most-significant byte is with binary-coded decimal format transmission area code, secondary most-significant byte with binary-coded decimal Format transmission bit code;The 16th data in each 32 data represent the validity of Hanzi section-position code, 1 effectively, 0 invalid.
More specifically embodiment:
According to way point database store structure inside step one inertial navigation system, the navigation of project way point database purchase is set up Parameter information;With 01 way point in No. 2 course lines, as a example by way point Chinese Xi'an:Way point title west is obtained by software Pacify corresponding Hanzi section-position code and be respectively 4687 and 1618, region-position code data message is pressed into way point structure information storage form, See accompanying drawing 2, stored.
Uc_wp_fp_no=2;/ * course lines number be 2*/
Ui_wp_no=01;/ * air routes period be 1*/
Uc_wp_name [1] [0]=46;1 area's code of/* way point titles word, West code 46.*/
Uc_wp_name [1] [1]=87;1 bit code of/* way point titles word, western bit code 87.*/
Uc_wp_name [2] [0]=16;2 area's code of/* way point titles word, peace area code 16.*/
Uc_wp_name [2] [1]=18;2 bit code of/* way point titles word, peace bit code 18.*/
Uc_wp_name [3] [0]=255;3 area's code of/* way point titles word, unused .*/
Uc_wp_name [3] [1]=255;3 bit code of/* way point titles word, unused */
Uc_wp_name [4] [0]=255;4 area's code of/* way point titles word, unused */
Uc_wp_name [4] [1]=255;4 bit code of/* way point titles word, unused .*/
The control instruction of No. 1 point in No. 2 course lines of inquiry of step 2 receive user, analysis instruction are intended to, and are adjusted according to command request The Chinese information stored in degree inquiry air route point data base.First, No. 2 course data storage startings are reduced to according to route information Address 0X8,010 0000;Secondly, according to air route period, get and change region way point skew 0X0,000 0000;Final should Way point information starting 0X8010 00,00+,0X0,000 0000, obtain way point information.
Step 4 by Chinese region-position code information " Xi'an ", according to Chinese information universal standard communications protocol format, can use by generation In the bus data of HB6096 bus transfers, the transmission of bus format Chinese data is completed, Fig. 3 is seen.
According to 4 32 BITBUS network data words of communications protocol generation transmission " Xi'an " it is:
0X2E57 0677;
0X1012 0678;
0XFFFF 0679;
0XFFFF 067A。
Step 5 control display unit receives the Chinese information of bus transfer, to the total of Chinese information universal standard communications protocol format , according to being parsed, the word that fetches data is high 16 for line number, and most most-significant byte is area's code, and secondary most-significant byte is bit code;Generate Chinese information correspondence Hanzi section-position code 4687 and 1618.
Step 6 is by conversion map method, area code code1, bit code code1, Chinese character digit hz_no in mark character library, the Chinese Starting position coordinates Len of the word in font file, Chinese character dot matrix buffering area hz_buff [32];Obtain Chinese character point methods as follows:
Hz_no=((code1&0x07f) * 94)+(code2&0x07f);
Len=hz_no*32L;
32 byte dot array datas are continuously read in hz_buff [32] from standard dot matrix word library HZK16 file Len positions, that is, is obtained The dot array data of the Chinese character.Chinese information " Xi'an " corresponding character lattice information is obtained according to the method, to Chinese character dot matrix according to According to display algorithm, carry out picture element scan and show to form Chinese Graphic.
It is as follows that Chinese character dot matrix presses picture element scan display methods;
By more than, operation realizes that user checks process Chinese Information application problem to inertial navigation system air route, improves navigation letter The display capabilities of breath, increased the convenience of user's manipulation.

Claims (2)

1. a kind of Chinese information display methods for inertial navigation system, described inertial navigation system include navigation component and control Display unit processed, be stored with navigation component air route point data base, and each the way point information in the point data base of air route includes this The region-position code of way point, longitude, latitude and height, the region-position code that is stored with control display unit dot array data storehouse, wherein Dot matrix of each region-position code to the Chinese geographic name that should have the position representation, it is characterised in that the method is comprised the following steps:
Navigation component judges that to the navigation information for gathering such as the navigation information of collection is coincide with certain way point information, then will The packet of the way point information is sent to control display unit, after control display unit receives way point information, region-position code is believed Breath is parsed, and obtains the corresponding dot matrix of the region-position code according to region-position code dot array data storehouse, and the dot array data is sent to aobvious Showing device is shown.
2. a kind of Chinese information display methods for inertial navigation system according to claim 1, it is characterised in that:Its In, the packet of the way point information is sent to control display unit by HB6096 buses by navigation component, and by foundation Chinese information universal standard communication protocol is communicated, and the Chinese information universal standard communication protocol is based on HB6096 bus protocols, State matrix and parity check bit are consistent with which, wherein, each packet have 4 32 data, first 32 Most least-significant byte index value in data is that 0X77 representative informations are Chinese character 1, the most least-significant byte index value in second 32 data It is Chinese character 2 for 0X78 representative informations, it is Chinese character 3 that the most least-significant byte index value in the 3rd 32 data is 0X79 representative informations, It is Chinese character 4 that most least-significant byte index value in 4th 32 data is 0X78 representative informations;It is high by 16 in each 32 data For transmitting Hanzi section-position code, most most-significant byte is with binary-coded decimal format transmission area code, secondary most-significant byte with binary-coded decimal format transmission bit code for position; The 16th data in each 32 data represent the validity of Hanzi section-position code, 1 effectively, 0 invalid.
CN201510575786.4A 2015-09-10 2015-09-10 Chinese information display method for inertial navigation system Pending CN106525032A (en)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1104322A (en) * 1994-08-31 1995-06-28 北京市中软计算机研究所 Communication type satellite navigation positioning instrument
CN1106596A (en) * 1994-04-22 1995-08-09 北京市赛达科贸公司 Electronic mapped GPS receiver
CN1770155A (en) * 2005-09-23 2006-05-10 赵忠华 Electronic map making and using method
CN102353966A (en) * 2011-07-13 2012-02-15 惠州Tcl移动通信有限公司 Navigator and navigation system
CN102594508A (en) * 2012-02-28 2012-07-18 厦门雅迅网络股份有限公司 Data transmission method for Beidou RDSS (radio determination satellite service) message receiving/transmitting
CN103986479A (en) * 2014-04-08 2014-08-13 河南工业大学 Electronic landmark device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1106596A (en) * 1994-04-22 1995-08-09 北京市赛达科贸公司 Electronic mapped GPS receiver
CN1104322A (en) * 1994-08-31 1995-06-28 北京市中软计算机研究所 Communication type satellite navigation positioning instrument
CN1770155A (en) * 2005-09-23 2006-05-10 赵忠华 Electronic map making and using method
CN102353966A (en) * 2011-07-13 2012-02-15 惠州Tcl移动通信有限公司 Navigator and navigation system
CN102594508A (en) * 2012-02-28 2012-07-18 厦门雅迅网络股份有限公司 Data transmission method for Beidou RDSS (radio determination satellite service) message receiving/transmitting
CN103986479A (en) * 2014-04-08 2014-08-13 河南工业大学 Electronic landmark device

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Application publication date: 20170322

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