JPH0415586A - Gps receiver - Google Patents

Gps receiver

Info

Publication number
JPH0415586A
JPH0415586A JP11869690A JP11869690A JPH0415586A JP H0415586 A JPH0415586 A JP H0415586A JP 11869690 A JP11869690 A JP 11869690A JP 11869690 A JP11869690 A JP 11869690A JP H0415586 A JPH0415586 A JP H0415586A
Authority
JP
Japan
Prior art keywords
antenna
satellites
antennas
satellite
reception
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
JP11869690A
Other languages
Japanese (ja)
Other versions
JP3020255B2 (en
Inventor
Toru Yoshihara
徹 吉原
Masashi Shimakata
島方 正志
Toshiaki Tsuchiya
利昭 土屋
Shigeru Tsujimura
辻村 滋
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.)
Pioneer Corp
Original Assignee
Pioneer Electronic Corp
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 Pioneer Electronic Corp filed Critical Pioneer Electronic Corp
Priority to JP2118696A priority Critical patent/JP3020255B2/en
Priority to US07/657,784 priority patent/US5248981A/en
Priority to EP91102628A priority patent/EP0455943B1/en
Priority to DE69121455T priority patent/DE69121455T2/en
Publication of JPH0415586A publication Critical patent/JPH0415586A/en
Application granted granted Critical
Publication of JP3020255B2 publication Critical patent/JP3020255B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

PURPOSE:To hold a satisfactory receiving state even when a satellite is obstructed by an obstacle by providing plural pieces of antennas, switching and controlling an antenna switching means, and selecting the antenna whose number of receivable satellites is maximum. CONSTITUTION:Plural antennas 1A, 1B are installed in positions separated to the utmost. When reception of a GPS satellite is started, a control part 5 controls an antenna switch 2, selects alternately the antennas 1A, 1B, sends receiving radio waves of the respective antennas to an RF receiving part 3 and a signal processing part 4, and derives the number of receivable satellites of the respective antennas. Subsequently, the control part 5 compares the obtained satellite numbers. When the antenna 1A (1B) is larger in the number of receivable satellites, the switch 2 is switched to the antenna 1A (1B) side, and reception of the satellite is executed by using the antenna 1A (1B). The control part 5 executes repeatedly the processing at every prescribed interval. As a result, even if the satellite whose position is being measured is obstructed by a building, etc., and becomes unreceivable, the position measurement can be continued by using other receivable satellite.

Description

【発明の詳細な説明】 (産業−1−の利用分野〕 本発明し1、人工衛星を用いた測位システムであるにP
S (GIobi+I Positioning Sy
stem)を利用し7て測イ☆を行うG P S受信機
に関する。
[Detailed Description of the Invention] (Field of Application of Industry-1-) The present invention is a positioning system using an artificial satellite.
S (GIobi+I Positioning Sy
The present invention relates to a GPS receiver that performs measurements using 7 stems.

〔従来の技術I G P Sを利用して測位を行うには、14低;)個、
望まし2くは4個のC,I’ S衛星を必要さ′、(イ
ζ)、 一般に、車載用ナヒケーシ・!ン装置などで使
用さ、11.るG P S受イ11機は、1チャンネル
構成の受信機に1つの7ンデナを備え、測位に必要な個
数以上の所望数の衛星をシーケンシャル受信しているの
が))IL通である。
[To perform positioning using conventional technology IGPS, 14 low;) pieces;
Preferably, two or four C, I'S satellites are required (Iζ); 11. The 11 GPS receivers are equipped with one seven-channel receiver and are capable of sequentially receiving a desired number of satellites, which is more than the number required for positioning.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

しかしながら、従来のように1つのアンテナで複数のG
r)S衛斤を受信する場合、衛〒がヒルなどて遮られる
七、測位に必要な規定数の衛星を受信できないことがあ
った。このような問題は、車両の移動を伴う車載用GP
S受信機において特に顕著である。
However, as in the past, one antenna can handle multiple G
r) When receiving S satellites, the satellites were sometimes blocked by hills, etc., and sometimes it was not possible to receive the specified number of satellites required for positioning. Such problems arise when using an in-vehicle GP that involves movement of the vehicle.
This is particularly noticeable in S receivers.

本発明は、上記問題を解決するためになされたもので、
その目的とするところは、障害物によって衛星が遮られ
た場合でも、できるだけ良好な受信状態を保つことがで
きるようしたGPS受信機を提供することである。
The present invention was made to solve the above problems, and
The objective is to provide a GPS receiver that can maintain as good reception as possible even when the satellites are blocked by obstacles.

〔課題を解決するだめの手段〕[Failure to solve the problem]

前記目的を達成するため、第1の発明は、1チャンネル
構成のGPS受信機において、複数本のアンテナと、該
複数本のアンテナを切換選択するアンテナ切換手段と、
該アンテナ切換手段を切り換え制御して受信可能な衛星
数が最大のアンテナを選択する手段とを備えたものであ
る。
In order to achieve the above object, a first invention provides a GPS receiver with a one-channel configuration, comprising: a plurality of antennas; an antenna switching means for switching and selecting the plurality of antennas;
and means for controlling the switching of the antenna switching means to select the antenna that can receive the maximum number of satellites.

また、第2の発明は、1ヂヤンネル構成のGPS受信機
において、複数本のアンテナと、該複数本のアンテナを
切換選択するアンテナ切換手段と、すべてのアンテナか
rめ定めた受信衛星最低数以下の衛星しか受信できなく
なったとき、それぞれのアンテナで受信可能な全衛星中
から測位に適した所定数の衛星を選択し、前記アンテナ
切換手段を切り換え制御して該選択した衛星に対応する
アンテナを順次選択する手段とを備えたものである。
Further, a second invention provides a GPS receiver having a one-channel configuration, including a plurality of antennas, an antenna switching means for switching and selecting the plurality of antennas, and a method in which all the antennas are arranged to be less than or equal to a predetermined minimum number of reception satellites. When only one satellite can be received, a predetermined number of satellites suitable for positioning are selected from among all the satellites that can be received by each antenna, and the antenna switching means is switched and controlled to switch the antenna corresponding to the selected satellite. and means for sequentially selecting.

〔作 用〕[For production]

第1の発明の場合、複数のアンテナのうち、最も受信状
態のよいアンテナを用いて衛星の受信が行われる。した
がって、より多くの衛星を受信することができ、一部の
衛星がビルなどで遮られた場合でも、他の受信衛星を用
いて測位を続行することができる。
In the case of the first invention, satellite reception is performed using the antenna with the best reception condition among the plurality of antennas. Therefore, more satellites can be received, and even if some satellites are blocked by buildings, positioning can be continued using other receiving satellites.

第2の発明の場合、すべてのアンテナの受信衛星数が予
め定めた受信衛星最低数以下まで低下したとき、各アン
テナの受信可能な全衛星中から測位に適した所定の数の
衛星を選択して受信する。
In the case of the second invention, when the number of receiving satellites for all antennas falls below a predetermined minimum number of receiving satellites, a predetermined number of satellites suitable for positioning are selected from among all the satellites that can be received by each antenna. and receive it.

したがって、個々のアンテナでは測位不可能な受信状態
となっても、アンテナ全体の受信衛星を利用して測位が
続行される。
Therefore, even if a reception state occurs in which positioning is not possible with each individual antenna, positioning can be continued using the receiving satellites of all the antennas.

なお、第2の発明における衛星の選択条件としては、例
えば、PDOP (幾何学的な精度劣化係数)の最も小
さな衛星の組め合わせ、あるいは受信信号強度の大きい
順に、所要個の衛星を選択すればよい。
Note that the conditions for selecting satellites in the second invention include, for example, selecting a combination of satellites with the smallest PDOP (geometric deterioration coefficient), or selecting the required number of satellites in order of the received signal strength. good.

〔実施例〕〔Example〕

以下、車載用GPS受信機の場合を例に採って本発明の
詳細な説明する。
Hereinafter, the present invention will be explained in detail by taking the case of a vehicle-mounted GPS receiver as an example.

第1図は本発明を適用して構成した車載用OPS受信機
の構成例を示す。図中、IA、IBは独立配置した2つ
のアンテナ、2はこの2つのアンテナを自在に切り換え
るアンテナ切換器、3は受信した衛星電波を逆拡散して
目的の衛星をシーケンシャル受信するRF受信部、4は
受信衛星の航法データから現在地の測位を行う信号処理
部、5は制御部である。なお、2つのアンテナIA、I
Bは、例えば第2図に示すように、車両のフロント側と
リア側など、できるだr、tHれた位置に設置すること
が望ましい。
FIG. 1 shows an example of the configuration of an on-vehicle OPS receiver configured to apply the present invention. In the figure, IA and IB are two independently arranged antennas, 2 is an antenna switcher that freely switches between these two antennas, 3 is an RF receiving unit that despreads the received satellite radio waves and sequentially receives the target satellite; 4 is a signal processing unit that positions the current location from the navigation data of the receiving satellite, and 5 is a control unit. In addition, two antennas IA, I
As shown in FIG. 2, for example, it is desirable to install B at positions as far apart as possible, such as the front and rear sides of the vehicle.

進んで、本発明の第1の実施例の動作を第3図のフじZ
−チャートを参照して説明する。
Proceeding, the operation of the first embodiment of the present invention will be explained as shown in FIG.
- Explain with reference to the chart.

GPS衛星の受信が開始されると(ステップ531)、
制御部5はアンテナ切換器2を制御してアンテナIA、
IBを交互に選択し、それぞれのアンテナの受信電波を
RF受信部3と信号処理部4に送り、アンテナLA、I
Bについてそれぞれのアンテナの受信可能な衛星数を求
める(ステップS32,533)。そして、制御部5は
、得られたアンテナIAとIBの受信可能衛星数を比較
する(ステップ534)。
When GPS satellite reception starts (step 531),
The control unit 5 controls the antenna switching device 2 to select the antennas IA,
IB is selected alternately, and the received radio waves of each antenna are sent to the RF receiving section 3 and signal processing section 4, and the antennas LA, I
For B, the number of satellites that can be received by each antenna is determined (steps S32, 533). Then, the control unit 5 compares the obtained number of satellites that can be received by the antennas IA and IB (step 534).

アンテナIAの方が受信可能な衛星数が多い場合、アン
テナ切換器2をアンテナ切換器に切り換え、アンテナI
Aを用いて衛星の受信を行う(ステップ535)。一方
、アンテナIBの方が受信可能な衛星数が多い場合、ア
ンテナ切換器2をアンテナ切換器に切り換え、アンテナ
1Bを用いて衛星の受信を行う(ステップ336)。
If the number of satellites that can be received by antenna IA is larger than that of antenna IA, switch antenna switch 2 to antenna switch
Satellite reception is performed using A (step 535). On the other hand, if the number of satellites that can be received by antenna IB is greater than that by antenna IB, antenna switching device 2 is switched to the antenna switching device, and satellite reception is performed using antenna 1B (step 336).

制御部5は前記処理を所定間隔毎に繰り返し実行ずイ)
。、−の結果、2つの、?ンラ)]A、lBの・)らの
受信iiJ能な衛星数の大きい側の7ンう°すを用いて
受信が行われ、測(i′f中の衛−星がビルなどで遮ら
4って受信不能となった場合でも、他の受信可能な衛〒
を用いて測位を続行することができる。
The control unit 5 repeatedly executes the process at predetermined intervals.
. As a result of ,-, two ? Reception is performed using the 7th channel on the side with the largest number of satellites that can be received by A, IB, etc., and if the satellite in the measurement (i'f) is blocked by a building Even if reception becomes impossible, you can use other satellites that can receive
Positioning can be continued using

第4図に本発明の第2の実施例の動作のフローチャート
を示す。なお、GPS受信機自体の構成は第1図と同様
である。
FIG. 4 shows a flowchart of the operation of the second embodiment of the present invention. Note that the configuration of the GPS receiver itself is the same as that shown in FIG.

この第2の実施例の場合、2つのアンう−J−IA。In the case of this second embodiment, two un-J-IAs.

I Bには予めそれぞれのアンテリー4TJ′tこ判定
しきい値たる受信衛星最低数(例えば5個など)が設定
され、第4図中のステップS4/I以下の判定処理に使
用される。
The minimum number of reception satellites (for example, 5) serving as a determination threshold for each antenna 4TJ't is set in advance in IB, and is used for the determination processing in steps S4/I and subsequent steps in FIG.

G l) S衛星の受信が開始されると(ステップ54
1)、制御部5はアンテナ切換器2を制御してアンテナ
LA、IBを交互に選択し、それぞれのアンテナの受信
電波をRF受信部3と信号処理部4に送り、アンテナI
 A 、 I Bについてそれぞれのアンテナの受信可
能な衛星数を求める(ステップS42,543)。そし
て、制御部5は、この得られたアンテナIA、IBの受
信可能衛星数かr)J)定メタ13il記受(1)衛j
i!、 WE低fi 、L、 リb 人A イiJ#’
;かを判定する(スう−ツブ544)。
G l) When reception of the S satellite starts (step 54
1) The control unit 5 controls the antenna switch 2 to alternately select the antennas LA and IB, sends the received radio waves of each antenna to the RF receiver 3 and the signal processing unit 4, and selects the antenna I.
The number of satellites that can be received by each antenna is determined for A, IB (steps S42, 543). Then, the control unit 5 calculates the number of satellites that can be received by the obtained antennas IA and IB.
i! , WE low fi, L, Lib person A iJ#'
(Step 544).

アンテナ1△、II3の受(P+可能衛11!数がとも
乙、二受()−衛r11最低数以トである場合、処理は
ステップS45へ移行し、アンテナ1ΔとIBのどちら
の力か受(、’; r−i1能衛早数が炙いかを判定し
、受信可能な衛h1数の多い側のアンテリ・て衛星の受
イハを行・)(ステップ346 、47)。
If the force of antenna 1△, II3 (P+possible force 11!) is equal to or greater than the minimum number of force of antenna 1△, II3 (P+possible force 11!), the process moves to step S45, and the force of antenna 1Δ or IB is determined. Receiving (,'; Determine whether the number of r-i1 satellites is hot or not, and perform reception of the antenna satellite with the larger number of receivable satellites (steps 346, 47).

・方、スウーンプS 44において、アンテナ1Δ。- On the other hand, in Swoop S44, antenna 1Δ.

11つかともに受信衛星最低数基1−でない場合、処理
はステップ348へ移行し、両方のアンテナかともに受
信衛星最低数取トζあるか否かが判定される。そして、
いずれか一方のアンテナのみが受信衛星最低数以下の場
合、処理はステップS 49・\移行し、いずれのアン
テナが受信衛星最低数基ドであるかを判定し、受信衛星
最低数以上となる側のアンテナを用いて衛にの受信を行
う(ステップS 50 + 5 ] )。
If the minimum number of receiving satellites for both antennas is not 1-, the process moves to step 348, and it is determined whether the minimum number of receiving satellites for both antennas is 1-. and,
If only one of the antennas has the minimum number of receiving satellites or less, the process moves to step S49, where it is determined which antenna has the minimum number of receiving satellites or more, and The satellite is received using the antenna (step S 50 + 5 ).

さらに、前記ステップS48において、アンテナ1Δと
I Bの両方がともに受信衛星最低数以下と判定された
場合、処理はステップS52へ移行する。そして、2つ
のアンテナIA、IBによって受信可能なすべての衛星
の中からその時点におlる測位に適した所定数の衛星を
選択する。
Further, if it is determined in step S48 that both antennas 1Δ and IB are equal to or less than the minimum number of receiving satellites, the process moves to step S52. Then, a predetermined number of satellites suitable for positioning at that time are selected from among all the satellites that can be received by the two antennas IA and IB.

この衛星の選択条件としては、前述したように、例えば
PDOP(XJ何学的な精度劣化係数)が最も小さくな
る衛星の組め合わせ、あるいは受信信号強度の大きい順
に、所定個数の衛星を選択すれはよい。
As mentioned above, the conditions for selecting satellites include, for example, selecting a combination of satellites with the smallest PDOP (XJ mathematical precision deterioration coefficient), or selecting a predetermined number of satellites in descending order of received signal strength. good.

前記のようにしてステップS52において所定数の衛星
が選択されると、制御部5ばこれに従ってアンテナ切換
器2を適応的に切り換え制御し、アンテナlΔとIBの
両者を用いて前記選択した複数個の衛星をシーケンシャ
ルに受信する。
When a predetermined number of satellites are selected in step S52 as described above, the control unit 5 adaptively switches and controls the antenna switching device 2 in accordance with the selection, and uses both antennas lΔ and IB to select the selected plurality of satellites. satellites sequentially.

制御部5は前記処理を所定間隔毎に繰り返し実行する。The control unit 5 repeatedly executes the process at predetermined intervals.

この結果、2つのアンテナのいづれもが予め定めた受信
衛星最低数以下の衛星しか受信できなくなった場合、ア
ンテナLA、IBで受信可能なすべての衛星中からその
時の測位に適した所定数の衛星を選択して受信が行われ
る。したがって、i’1lll (☆中の衛星がヒルな
どで遮られて受信不能となった場合でも、他の受信可能
な衛星を用いて測位を続行ずろごとができる。
As a result, if either of the two antennas can only receive satellites that are less than the predetermined minimum number of reception satellites, a predetermined number of satellites suitable for positioning at that time will be selected from among all the satellites that can be received by antennas LA and IB. is selected and reception is performed. Therefore, even if the satellite in i'1llll (☆) is blocked by a hill or the like and cannot be received, positioning can be continued using other receivable satellites.

なお、1);I記実施例乙:12木のアンテナを用いた
場合を例に採ったが、2木取1−設りてもよいことt、
L勿論である。また、第2実施例におりる判定のための
受イ菖衛IT、最低数は、各アンチ−ノー毎るこ異なろ
稙としてもよいし、全アンテナについて同−埴とし7て
もよい。いずれを採用するかはシス−0J−1、のイ1
様に応して決定すればよい。
Note that 1); Embodiment B of Section I: The case where a 12-wood antenna is used is taken as an example, but 2 wood antennas 1- may be installed.
L Of course. In addition, the minimum number of reception ITs for the determination in the second embodiment may be set to be different for each anti-no, or may be set to be the same for all antennas. Which one to adopt is cis-0J-1, No.1
You can decide according to your needs.

〔発明の効果] 以ト述・\たとごろから明らかなように、第10)発明
によるときは、袂数のアンチノー中から受信可能な衛星
数の最も多いアンテーノ〜を選択して衛星を受信ずろよ
うにし、また、第2の発明によるとン\は、各アンテリ
で受信可能tI′すべての衛星中から測位に適U7た所
定数の衛星を選択L7てや一イ、)する31、’) l
cし7たので、測位中の衛JiIがじルl(どで遮ら1
・1゜て受信できなくなったようt(場合でも、他の受
信衛星を用いて測イ1γを続行することができ、測位が
中断される、ことを防止できる。さらに、複数のアンテ
ナを用いて受信するため、アンテナの設置場所を工夫す
ることにより全力位をカバーすることができ、移動を佳
う車載用GPS受信機などにおいて特にその効果が大き
い。
[Effects of the Invention] As is clear from the above description, according to the 10th invention, the antenna with the largest number of receivable satellites is selected from among the antinos of the number of bands to receive the satellite. According to the second invention, a predetermined number of satellites suitable for positioning are selected from among all the satellites that can be received by each antenna. l
7, so Mamoru JII who was positioning was interrupted by 1
・Even if reception becomes impossible at 1°, positioning can be continued using other receiving satellites, and positioning can be prevented from being interrupted.Furthermore, by using multiple antennas, By carefully arranging the location of the antenna for reception, it is possible to cover the entire range, and this is particularly effective for mobile GPS receivers and the like.

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

第1図は本発明を適用j7て構成したりt載用G PS
受信機の1実施例のブロック図、 第2図はアンテナの設置例を示す図、 第3図は本発明の第1の実施例の動作のフローチャー1
・、 第4図は本発明の第2の実施例の動作のフローチャー1
−である。 lA、]B・・・アンテリ′、2・・・アンテナ切換器
、3・・・RF受信部、4・・・信ぢ処理部、5・・・
制御部。
Figure 1 shows a GPS system configured by applying the present invention.
A block diagram of one embodiment of the receiver, FIG. 2 is a diagram showing an example of antenna installation, and FIG. 3 is a flowchart 1 of the operation of the first embodiment of the present invention.
・, FIG. 4 is a flowchart 1 of the operation of the second embodiment of the present invention.
− is. lA, ]B... Antenna ', 2... Antenna switcher, 3... RF receiving section, 4... Signal processing section, 5...
control section.

Claims (2)

【特許請求の範囲】[Claims] (1)1チャンネル構成のGPS受信機において、複数
本のアンテナと、 該複数本のアンテナを切換選択するアンテナ切換手段と
、 該アンテナ切換手段を切り換え制御して受信可能な衛星
数が最大のアンテナを選択する手段とを備えたことを特
徴とするGPS受信機。
(1) In a GPS receiver with a one-channel configuration, a plurality of antennas, an antenna switching means for switching and selecting the plurality of antennas, and an antenna that can receive the maximum number of satellites by switching and controlling the antenna switching means. A GPS receiver characterized by comprising: means for selecting.
(2)1チャンネル構成のGPS受信機において、複数
本のアンテナと、 該複数本のアンテナを切換選択するアンテナ切換手段と
、 すべてのアンテナが予め定めた受信衛星最低数以下の衛
星しか受信できなくなったとき、それぞれのアンテナで
受信可能な全衛星中から測位に適した所定数の衛星を選
択し、前記アンテナ切換手段を切り換え制御して該選択
した衛星に対応するアンテナを順次選択する手段とを備
えたことを特徴とするGPS受信機。
(2) A GPS receiver with a one-channel configuration includes multiple antennas, an antenna switching means for switching and selecting the multiple antennas, and a system in which all antennas can only receive satellites that are less than or equal to a predetermined minimum number of reception satellites. means for selecting a predetermined number of satellites suitable for positioning from among all the satellites that can be received by each antenna, and controlling the antenna switching means to sequentially select antennas corresponding to the selected satellites; A GPS receiver characterized by:
JP2118696A 1990-05-10 1990-05-10 GPS receiver Expired - Lifetime JP3020255B2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2118696A JP3020255B2 (en) 1990-05-10 1990-05-10 GPS receiver
US07/657,784 US5248981A (en) 1990-05-10 1991-02-20 Apparatus and method for positioning of a gps receiver
EP91102628A EP0455943B1 (en) 1990-05-10 1991-02-22 Apparatus and method for positioning of a GPS receiver
DE69121455T DE69121455T2 (en) 1990-05-10 1991-02-22 Device and method for positioning a GPS receiver

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2118696A JP3020255B2 (en) 1990-05-10 1990-05-10 GPS receiver

Publications (2)

Publication Number Publication Date
JPH0415586A true JPH0415586A (en) 1992-01-20
JP3020255B2 JP3020255B2 (en) 2000-03-15

Family

ID=14742897

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2118696A Expired - Lifetime JP3020255B2 (en) 1990-05-10 1990-05-10 GPS receiver

Country Status (1)

Country Link
JP (1) JP3020255B2 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007180884A (en) * 2005-12-27 2007-07-12 Kyocera Corp Wireless communication apparatus and wireless communication system
JP2007180883A (en) * 2005-12-27 2007-07-12 Kyocera Corp Wireless communication apparatus and wireless communication control method of wireless communication apparatus
JP2014089190A (en) * 2009-06-24 2014-05-15 Qualcomm Incorporated Receive diversity in gnss receivers

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007180884A (en) * 2005-12-27 2007-07-12 Kyocera Corp Wireless communication apparatus and wireless communication system
JP2007180883A (en) * 2005-12-27 2007-07-12 Kyocera Corp Wireless communication apparatus and wireless communication control method of wireless communication apparatus
JP4689463B2 (en) * 2005-12-27 2011-05-25 京セラ株式会社 Wireless communication apparatus and wireless communication control method for wireless communication apparatus
JP2014089190A (en) * 2009-06-24 2014-05-15 Qualcomm Incorporated Receive diversity in gnss receivers
JP2015083983A (en) * 2009-06-24 2015-04-30 クゥアルコム・インコーポレイテッドQualcomm Incorporated Receive diversity in gnss receivers

Also Published As

Publication number Publication date
JP3020255B2 (en) 2000-03-15

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