JPS61198073A - Gps receiving device - Google Patents

Gps receiving device

Info

Publication number
JPS61198073A
JPS61198073A JP3954485A JP3954485A JPS61198073A JP S61198073 A JPS61198073 A JP S61198073A JP 3954485 A JP3954485 A JP 3954485A JP 3954485 A JP3954485 A JP 3954485A JP S61198073 A JPS61198073 A JP S61198073A
Authority
JP
Japan
Prior art keywords
data
time
orbit data
turned
reception processing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP3954485A
Other languages
Japanese (ja)
Other versions
JPH0262187B2 (en
Inventor
Noboru Yamaoka
山岡 登
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Japan Radio Co Ltd
Original Assignee
Japan Radio Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Japan Radio Co Ltd filed Critical Japan Radio Co Ltd
Priority to JP3954485A priority Critical patent/JPS61198073A/en
Publication of JPS61198073A publication Critical patent/JPS61198073A/en
Publication of JPH0262187B2 publication Critical patent/JPH0262187B2/ja
Granted legal-status Critical Current

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  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

PURPOSE:To measure quickly the present position of a moving body, when a power source has been turned on, by providing a track data availability discriminating means, etc., and executing position measurement from stored track data, when the recollection has become unnecessary. CONSTITUTION:A radio wave from a GPS satellite is received by a reception processing part 12, and track data, etc. of each satellite are calculated and stored in a reception processing part use memory 14. On the other hand, time data of the track data is stored in a track data collecting time memory 16. When a power source is turned on again after the power source has been cut off, a collection time data T1 of the previous time and the present time data T2 are read out, and supplied to a track data availability discriminator 22. In this state, when a signal for making a recollection of the track data unnecessary has been received in the discriminator 22, the reception processing part 12 executes position measurement by the data which has been collected and stored before the power source is cut off. As a result, the collecting of the track data is unnecessary, and the position measurement can be executed quickly from the time when the power source is turned on.

Description

【発明の詳細な説明】 本発明はGrobal Positioning Sy
stem (以下GPSと称する)を利用した受信装置
に関し、一層詳細には、特に電源投入時に速やかに船舶
、自動車等の現在位置の測位を行うことを可能にしたG
PS受信装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention is based on Global Positioning Systems.
Regarding receiving devices using GPS (hereinafter referred to as GPS), in more detail, GPS is a GPS system that makes it possible to quickly determine the current position of ships, automobiles, etc. when the power is turned on.
This invention relates to a PS receiving device.

船舶や航空機のような時々刻々移動する利用者に対し、
複数個の人工衛星から電波を送給してその現在位置、走
行速度等を確認乃至決定するために、近年、GPS測位
装置の存効性が注目を浴びている。このGPS測位装置
は、■ 全世界でいつでも連続して利用出来る、■ 位
置、速度の測定精度が極めて高い、■ 利用者数に制限
がない 等の特徴を備えている。
For users who move from time to time, such as ships and aircraft,
In recent years, the effectiveness of GPS positioning devices has been attracting attention because they transmit radio waves from a plurality of artificial satellites to confirm or determine their current positions, traveling speeds, and the like. This GPS positioning device has the following characteristics: (1) It can be used continuously all over the world at any time, (2) It has extremely high accuracy in measuring position and speed, and (2) There is no limit to the number of users.

このような観点からすれば、GPS測位装置を利用する
客体は船舶、航空機に限ることなく、自動車もその対象
となって然るべきである。特に、都市部の交通の混雑を
回避し、短時間に自らの現在位置を確認し、目的地まで
の迂回路を発見する等に利用出来れば、時間的、経済的
に頗る大きな効果が得られよう。
From this point of view, objects using GPS positioning devices are not limited to ships and aircraft, but should also include automobiles. In particular, if it can be used to avoid traffic congestion in urban areas, confirm one's current location in a short time, and find detours to a destination, it can have significant time and economic benefits. Good morning.

ところで、従来のGPS受信装置においては、電源の投
入によりGPS衛星の軌道データ暦から3乃至4個のG
PS衛星を選択し、選択した衛星からの信号を受信して
その軌道データを収集した後に位置測定を行っている。
By the way, in conventional GPS receivers, when the power is turned on, three to four G
Positioning is performed after selecting a PS satellite, receiving signals from the selected satellite, and collecting orbit data.

このため、電源投入時から位置測定までにGPS衛星の
軌道データの収集等のためにかなりの時間を必要とし、
電源投入時から測位まで相当な待機時間がかかる欠点が
あった。このことは、例えば、GPS受信装置により自
動車の位置を測定するような場合に、電源投入時に直ち
に測位出来ないという不都合として露呈する。
For this reason, it takes a considerable amount of time to collect GPS satellite orbit data from the time the power is turned on until the position is measured.
The disadvantage is that it takes a considerable amount of time to wait from when the power is turned on until positioning is determined. For example, when the position of a car is measured using a GPS receiving device, this becomes an inconvenience in that the positioning cannot be performed immediately when the power is turned on.

本発明は前記の不都合を克服するためになされたもので
あって、GPS受信機に電源が投入された時、その前の
電源遮断直前に収集されたGPS衛星の軌道データの収
集時刻と、リアルタイムクロックによる現在時刻とから
前回収集した軌道データが現在の測位計算に使用可能か
どうか判断し、使用可能の場合に、電源投入後、GPS
衛星の軌道データの収集を省略し、前回収集した軌道デ
ータを用いて現位置の測位をすることを可能にするGP
S受信装置を提供することを目的とする。
The present invention has been made in order to overcome the above-mentioned disadvantages, and the present invention has been made to enable the collection time and real time of the orbit data of the GPS satellites collected immediately before the previous power cut-off, when the power is turned on to the GPS receiver. It is determined whether the previously collected orbit data can be used for the current positioning calculation based on the current time according to the clock, and if it can be used, after the power is turned on, the GPS
GP that makes it possible to omit the collection of satellite orbit data and measure the current position using the previously collected orbit data
The purpose of the present invention is to provide an S receiving device.

前記の目的を達成するために、本発明はGPS衛星から
の電波を受信して位置を計測するGPS受信装置におい
て、GPS衛星の軌道データを受信収集した時刻を記憶
し且つ電源遮断時バックアップされる軌道データ収集時
刻記憶手段と、前記軌道データを記憶し且つ電源遮断時
もバックアップされる軌道データ記憶手段と、電源遮断
時もバックアップされて実時刻を記憶する実時間クロッ
クと、電源投入の時前記実時間クロックから出力された
実時刻と軌道データ収集時刻記憶手段から読み出した時
刻との差が所定値内か否かにより軌道データの再収集の
要・不要を判断する軌道データ使用可否判別手段とを備
え、前記軌道データ使用可否判断手段の出力により再収
集不要とされた時前記軌道データ記憶手段から読み出し
た軌道データから測位を行い、一方、前記軌道データの
再収集が必要とされた時、新たに軌道データを収集しこ
の収集軌道データから測位を行うことを特徴とする。
In order to achieve the above object, the present invention provides a GPS receiving device that receives radio waves from GPS satellites and measures the position, which stores the time at which the orbital data of the GPS satellites is received and collected, and which is backed up when the power is cut off. orbit data collection time storage means; orbit data storage means that stores the orbit data and is backed up even when the power is turned off; a real time clock that is backed up and stores the real time even when the power is turned off; orbit data usability determining means for determining whether re-collection of orbit data is necessary or unnecessary based on whether the difference between the real time output from the real time clock and the time read from the orbit data collection time storage means is within a predetermined value; When it is determined that re-collection is not necessary by the output of the orbit data usability determination means, positioning is performed from the orbit data read from the orbit data storage means, and on the other hand, when re-collection of the orbit data is required, The feature is that new orbit data is collected and positioning is performed from this collected orbit data.

次に、本発明に係るGPS受信装置について好適な実施
例を挙げ、添付の図面を参照しながら以下詳細に説明す
る。
Next, preferred embodiments of the GPS receiving device according to the present invention will be described in detail with reference to the accompanying drawings.

先ず、第1図に本発明の一実施例の構成を示すブロック
図を示す。
First, FIG. 1 shows a block diagram showing the configuration of an embodiment of the present invention.

そこで、アンテナ10の出力側は受信処理部12に接続
し、この受信処理部12の出力側は受信処理部用メモリ
14、軌道データ収集時刻メモリ16、表示部18およ
びリアルタイムクロック20に接続する。一方、前記受
信処理部用メモ1月4は記憶内容を受信処理部12に送
給すべく接続されると共に軌道データ使用可否判別器2
2の出力側は前記受信処理部12に接続している。なお
、前記軌道データ収集時刻メモリ16並びにリアルタイ
ムクロック20の出力側は前記軌道データ可否判別器2
2に接続しておく。
Therefore, the output side of the antenna 10 is connected to a reception processing section 12, and the output side of this reception processing section 12 is connected to a reception processing section memory 14, an orbit data collection time memory 16, a display section 18, and a real-time clock 20. On the other hand, the memo 4 for the reception processing section is connected to send the stored contents to the reception processing section 12, and the orbit data usability discriminator 2
The output side of 2 is connected to the reception processing section 12. Note that the output side of the orbit data collection time memory 16 and the real-time clock 20 is connected to the orbit data availability discriminator 2.
Connect it to 2.

そこで、アンテナ10を介して複数個のGPS衛星(図
示せず)から送給される信号は受信信号から各衛星の軌
道データ収集と各衛星からアンテナ10までの擬似距離
等を測定する受信処理部12に供給される。受信処理部
12は収集した軌道データおよび測位擬似距離データを
受信処理部用メモリ14に供給して記憶させると共に、
軌道データ収集時刻を軌道データ収集時刻メモリ16に
供給して記憶させ、これらのデータから高精度且つ瞬時
に位置、高度、時刻等を計測する。
Therefore, signals sent from a plurality of GPS satellites (not shown) via the antenna 10 are processed by a reception processing unit that collects orbit data of each satellite from the received signal and measures pseudo distances from each satellite to the antenna 10. 12. The reception processing unit 12 supplies the collected trajectory data and positioning pseudorange data to the reception processing unit memory 14 for storage, and
The orbit data collection time is supplied to the orbit data collection time memory 16 and stored, and the position, altitude, time, etc. are measured with high precision and instantaneously from this data.

次いで、受信処理部12で計測したデータを表示部1日
に供給して数値表示、または、地図図形上の航跡として
表示する。また、受信処理部用メモ1月4および軌道デ
ータ収集時刻メモリ16は、例えば、蓄電池によりバッ
クアップしてあって、電源遮断中においても記憶動作を
維持する。
Next, the data measured by the reception processing section 12 is supplied to the display section 1 and displayed numerically or as a track on a map figure. Further, the memo 4 for the reception processing section and the orbit data collection time memory 16 are backed up by, for example, a storage battery, and maintain storage operations even during power cutoff.

一方、リアルタイムクロック20は受信処理部I2で計
測された時刻情報に基づいて較正され、且つ、例えば、
蓄電池によってバックアップしてあり、電源遮断中にお
いても記憶動作を維持する。軌道データ収集時刻メモリ
16における記憶収集時刻データとリアルタイムクロッ
ク20からの時刻データとは、電源投入時に前回収集し
た軌道データを現在における測位計算に使用可能か否か
を判別する軌道データ使用可否判別器22に供給し、こ
の軌道データ使用可否判別器22の判別出力は受信処理
部12に供給しである。
On the other hand, the real-time clock 20 is calibrated based on time information measured by the reception processing unit I2, and, for example,
It is backed up by a storage battery and maintains memory operation even when the power is cut off. The stored collection time data in the orbit data collection time memory 16 and the time data from the real-time clock 20 are used as an orbit data usability discriminator that determines whether or not the previously collected orbit data can be used for the current positioning calculation when the power is turned on. 22, and the determination output of this orbit data usability determiner 22 is supplied to the reception processing section 12.

次に、以上のように構成される本発明の作用について、
第2図に示すフローチャートに沿ってさらに詳細に説明
する。
Next, regarding the operation of the present invention configured as above,
This will be explained in more detail along the flowchart shown in FIG.

GPS衛星からの電波はアンテナ10を介して受信処理
部12によって受信され、受信処理部12において増幅
、復調され、復調データが演算処理されて復調データか
ら各衛星の軌道データ、擬似距離データが演算され、こ
れらのデータは受信処理部用メモリ14に記憶される。
Radio waves from GPS satellites are received by the reception processing unit 12 via the antenna 10, amplified and demodulated in the reception processing unit 12, the demodulated data is subjected to arithmetic processing, and orbit data and pseudorange data of each satellite are calculated from the demodulated data. These data are stored in the reception processing unit memory 14.

また、受信処理部用メモリ14から読み出されたデータ
から瞬時に位置、高度、時刻データが演算され、この演
算されたデータは表示部18に供給され、当該表示部1
日において数値表示または地図図形上の航跡として表示
されることは前記の通りである。
Further, position, altitude, and time data are instantaneously calculated from the data read out from the memory 14 for the reception processing unit, and this calculated data is supplied to the display unit 18.
As mentioned above, the date is displayed numerically or as a track on a map.

一方、受信処理部12による演算処理において得られた
各衛星の軌道データは受信処理部用メモリ14に記憶さ
れ、軌道データが収集された時の時刻データは軌道デー
タ収集時刻メモリ16に記憶される。
On the other hand, the orbit data of each satellite obtained through the arithmetic processing by the reception processing section 12 is stored in the reception processing section memory 14, and the time data when the orbit data was collected is stored in the orbit data collection time memory 16. .

そこで、今、必要とする測位が終わって電源が遮断され
た時においても、受信処理部用メモIJ14の記憶内容
、軌道データ収集時刻メモリ16の記憶内容およびリア
ルタイムクロック20のクロックデータは、前記の通り
、蓄電池によるバックアンプのために維持されている。
Therefore, even when the necessary positioning is completed and the power is cut off, the memory contents of the reception processing section memo IJ14, the memory contents of the orbit data collection time memory 16, and the clock data of the real-time clock 20 are retained as described above. As expected, it is maintained for back-up amplification by storage batteries.

電源遮断の後、再度電源が投入された時、第2図のフロ
ーチャートに示すように、軌道データ収集時刻メモリ1
6に記憶されている前回の収集時刻データT、が読み出
され(ステップa)、リアルタイムクロック20から現
時刻データT2が読み出されて(ステップb)、これら
は軌道データ使用可否判別器22に供給される。そして
、軌道データ使用可否判別器22において収集時刻から
現時刻までの経過時間ΔT、すなわちT2−T、=ΔT
のデータが算出される(ステップC)。
When the power is turned on again after the power is cut off, as shown in the flowchart in Figure 2, the orbit data collection time memory 1
The previous collection time data T stored in the real-time clock 20 is read out (step a), and the current time data T2 is read out from the real-time clock 20 (step b). Supplied. Then, in the trajectory data usability discriminator 22, the elapsed time ΔT from the collection time to the current time, that is, T2−T, =ΔT
data is calculated (step C).

軌道データ使用可否判別器22において、さらに、当該
cps受信装置搭載移動物体に対応して予め設定しであ
る軌道データ再収集許容経過時間T3と経過時間ΔTと
の大小が比較される(ステップd)。ステップdにおい
て、軌道データ使用可否判別器22からΔT≦T、の時
は受信処理部12へ軌道データの再収集が不要である旨
の信号が出力され(ステップe)、一方、ΔT≦T、の
時は受信処理部12へ軌道データの再収集が必要である
旨の信号が出力される(ステップf)。
The orbit data usability determiner 22 further compares the magnitude of the orbit data re-collection permissible elapsed time T3 and the elapsed time ΔT, which are preset corresponding to the moving object equipped with the CPS receiver (step d). . In step d, when ΔT≦T, the trajectory data availability discriminator 22 outputs a signal to the reception processing unit 12 indicating that re-collection of trajectory data is unnecessary (step e); on the other hand, if ΔT≦T, At this time, a signal indicating that re-collection of trajectory data is necessary is output to the reception processing section 12 (step f).

従って、ステップeにより軌道データの再収集が不要で
ある旨の信号を受けた受信処理部12は、電源遮断前に
おいて収集され且つ受信処理部用メモリ14に記憶され
ている各衛星の軌道データにより測位が行われる。この
結果、軌道データを収集する必要はなく、電源投入時か
ら速やかに測位をすることが出来る。
Therefore, the reception processing unit 12 that received the signal that re-collection of orbit data is unnecessary in step e uses the orbit data of each satellite that was collected before the power was cut off and stored in the reception processing unit memory 14. Positioning is performed. As a result, there is no need to collect orbit data, and positioning can be performed immediately after power is turned on.

また、ステップfによって軌道データ再収集が必要であ
る旨の信号を受けた時は、受信処理部12は複数個のG
PS衛星からの信号を受信し、軌道データを収集して、
収集軌道データから測位をすることになる。
Further, when receiving a signal indicating that trajectory data re-collection is necessary in step f, the reception processing unit 12 collects a plurality of G
Receive signals from PS satellites and collect orbit data,
Positioning will be done from the collected orbit data.

以上説明したように、本発明によれば、軌道データ再収
集許容経過時間(T3)≧経過時間(ΔT)の時は、電
源投入前における記憶済軌道データが使用出来、各衛星
からの軌道データを収集する必要はなく、従って、電源
投入時、速やかに移動体の現在位置が測定出来る。
As explained above, according to the present invention, when the orbit data re-collection allowable elapsed time (T3)≧the elapsed time (ΔT), the stored orbit data before power-on can be used, and the orbit data from each satellite can be used. Therefore, when the power is turned on, the current position of the moving object can be immediately measured.

また、本発明のGPS受信装置を自動車に搭載した時、
電源投入から速やかに自動車の現位置の測定が出来るこ
とになる。
Furthermore, when the GPS receiving device of the present invention is mounted on a car,
This means that the current position of the vehicle can be measured immediately after the power is turned on.

以上、本発明について好適な実施例を挙げて説明したが
、本発明はこの実施例に限定されるものではなく、本発
明の要旨を逸脱しない範囲において種々の改良並びに設
計の変更が可能なことは勿論である。
Although the present invention has been described above with reference to preferred embodiments, the present invention is not limited to these embodiments, and various improvements and changes in design can be made without departing from the gist of the present invention. Of course.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明の一実施例の構成を示すブロック図、第
2図は本発明の一実施例の作用説明に供するフローチャ
ートである。 10・・アンテナ    12・・受信処理部14・・
受信処理部用メモリ 16・・軌道データ収集時刻メモリ 18・・表示部 20・・リアルタイムクロック
FIG. 1 is a block diagram showing the configuration of an embodiment of the present invention, and FIG. 2 is a flowchart for explaining the operation of the embodiment of the present invention. 10...Antenna 12...Reception processing unit 14...
Reception processing unit memory 16...orbit data collection time memory 18...display unit 20...real-time clock

Claims (1)

【特許請求の範囲】[Claims] (1)GPS衛星からの電波を受信して位置を計測する
GPS受信装置において、GPS衛星の軌道データを受
信収集した時刻を記憶し且つ電源遮断時バックアップさ
れる軌道データ収集時刻記憶手段と、前記軌道データを
記憶し且つ電源遮断時もバックアップされる軌道データ
記憶手段と、電源遮断時もバックアップされて実時刻を
記憶する実時間クロックと、電源投入の時前記実時間ク
ロックから出力された実時刻と軌道データ収集時刻記憶
手段から読み出した時刻との差が所定値内か否かにより
軌道データの再収集の要・不要を判断する軌道データ使
用可否判別手段とを備え、前記軌道データ使用可否判断
手段の出力により再収集不要とされた時前記軌道データ
記憶手段から読み出した軌道データから測位を行い、一
方、前記軌道データの再収集が必要とされた時、新たに
軌道データを収集しこの収集軌道データから測位を行う
ことを特徴とするGPS受信装置。
(1) In a GPS receiving device that measures a position by receiving radio waves from a GPS satellite, an orbit data collection time storage means that stores the time at which the orbit data of the GPS satellite is received and is backed up when the power is cut off; an orbit data storage means that stores orbit data and is backed up even when the power is turned off; a real time clock that is backed up and stores the real time even when the power is turned off; and a real time that is output from the real time clock when the power is turned on. and a trajectory data usability determination means for determining whether re-collection of the trajectory data is necessary or unnecessary based on whether or not the difference between the time and the time read from the trajectory data collection time storage means is within a predetermined value. When it is determined that re-collection is not necessary based on the output of the means, positioning is performed from the orbit data read out from the orbit data storage means, while when it is necessary to re-collect the orbit data, new orbit data is collected and this collection is performed. A GPS receiving device characterized by performing positioning from orbit data.
JP3954485A 1985-02-28 1985-02-28 Gps receiving device Granted JPS61198073A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3954485A JPS61198073A (en) 1985-02-28 1985-02-28 Gps receiving device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3954485A JPS61198073A (en) 1985-02-28 1985-02-28 Gps receiving device

Publications (2)

Publication Number Publication Date
JPS61198073A true JPS61198073A (en) 1986-09-02
JPH0262187B2 JPH0262187B2 (en) 1990-12-25

Family

ID=12555993

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3954485A Granted JPS61198073A (en) 1985-02-28 1985-02-28 Gps receiving device

Country Status (1)

Country Link
JP (1) JPS61198073A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03269385A (en) * 1990-03-20 1991-11-29 Pioneer Electron Corp Gps receiver
JP2008197084A (en) * 2007-02-14 2008-08-28 O2 Micro Inc Gps receiver
WO2009016784A1 (en) * 2007-07-30 2009-02-05 Mitsubishi Electric Corporation Navigation system
JP2010139507A (en) * 1996-03-08 2010-06-24 Snaptrack Inc Advanced gps receiver using communication link

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03269385A (en) * 1990-03-20 1991-11-29 Pioneer Electron Corp Gps receiver
JP2010139507A (en) * 1996-03-08 2010-06-24 Snaptrack Inc Advanced gps receiver using communication link
JP2008197084A (en) * 2007-02-14 2008-08-28 O2 Micro Inc Gps receiver
WO2009016784A1 (en) * 2007-07-30 2009-02-05 Mitsubishi Electric Corporation Navigation system

Also Published As

Publication number Publication date
JPH0262187B2 (en) 1990-12-25

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