JP2699740B2 - Radar equipment - Google Patents

Radar equipment

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Publication number
JP2699740B2
JP2699740B2 JP34236491A JP34236491A JP2699740B2 JP 2699740 B2 JP2699740 B2 JP 2699740B2 JP 34236491 A JP34236491 A JP 34236491A JP 34236491 A JP34236491 A JP 34236491A JP 2699740 B2 JP2699740 B2 JP 2699740B2
Authority
JP
Japan
Prior art keywords
azimuth
amplitude
output
angle
monopulse
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.)
Expired - Lifetime
Application number
JP34236491A
Other languages
Japanese (ja)
Other versions
JPH05150036A (en
Inventor
誠二 野本
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.)
NEC Corp
Original Assignee
NEC 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 NEC Corp filed Critical NEC Corp
Priority to JP34236491A priority Critical patent/JP2699740B2/en
Publication of JPH05150036A publication Critical patent/JPH05150036A/en
Application granted granted Critical
Publication of JP2699740B2 publication Critical patent/JP2699740B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は捜索レーダ装置に関し、
特に方位に関してモノパルス測角処理を行うことにより
目標の方位角情報を得るレーダ装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a search radar system,
In particular, the present invention relates to a radar device that obtains target azimuth information by performing monopulse angle measurement processing on the azimuth.

【0002】[0002]

【従来の技術】従来、この種のレーダ装置は、目標の3
次元位置情報を得るため、所定のビーム走査プログラム
に従ってペンシルビームを方位及び仰角方向に走査して
いた。例えば、捜索レーダ装置の場合、広範囲の空間を
捜索するために、同一方位の各仰角毎に隣接する複数の
ペンシルビームを逐次形成し、これを水平面内で回転さ
せる方法が使われる。又、追尾レーダの場合、目標の精
密な3次元位置情報を得るために連続的に目標にペンシ
ルビームを照射する。
2. Description of the Related Art Conventionally, this type of radar apparatus has a target of 3
In order to obtain dimensional position information, the pencil beam has been scanned in azimuth and elevation directions according to a predetermined beam scanning program. For example, in the case of a search radar apparatus, a method of sequentially forming a plurality of adjacent pencil beams at each elevation angle in the same direction and rotating the pencil beams in a horizontal plane is used to search a wide area. In the case of a tracking radar, the target is continuously irradiated with a pencil beam in order to obtain precise three-dimensional position information of the target.

【0003】図2は従来のレーダ装置の構成例を示す。
このレーダ装置では、先ず、必要とする方向にビーム走
査を行うために、ビーム方向制御器1においてビーム方
向制御信号を発生し、空中線2へ出力する。空中線2
、図5(a)のように、ビーム方向制御信号に従っ
て、指定された方向にペンシルビームを形成する。この
とき、方位方向に隣り合ったビームを方位隣接ビームと
称する。方位測角をモノパルス方式で行うために、空中
線2は図3に示すような和パターンと差パターンの2種
類のビームパターンを同時に空間に形成する。空中線2
からの受信信号は、受信機3において高周波から中間周
波に変換された後、信号処理器4へ出力される。信号処
理器4では、目標以外の受信信号に対する抑圧処理を行
った後、受信信号の中から一定レベル以上の信号を目標
からの反射信号と判定し、振幅比較器5及び記憶器7へ
出力する。図5(b)示すように、記憶器7は現在の方
位より過去に走査した方位隣接ビームにおける目標信号
(1方位前のビームで受信された目標信号の和ビデオ)
を振幅比較器5に出力する。振幅比較器5は、現在の方
位の目標信号と過去に走査した方位隣接ビームにおける
目標信号の和ビデオを比較して後者の方が大きい場合、
モノパルス測角演算器6へ出力する。モノパルス測角演
算器6では、目標信号に対してモノパルス測角処理によ
り方位角を算出し、出力する。
FIG. 2 shows a configuration example of a conventional radar apparatus.
In this radar apparatus, first, in order to perform beam scanning in a required direction, a beam direction controller 1 generates a beam direction control signal and outputs the signal to the antenna 2. Antenna 2
Forms a pencil beam in a designated direction according to a beam direction control signal as shown in FIG . this
When the beam adjacent in the azimuth direction is
Name. In order to perform the azimuth measurement by the monopulse method, the antenna 2 simultaneously forms two types of beam patterns, that is, a sum pattern and a difference pattern as shown in FIG. Antenna 2
Is converted from a high frequency to an intermediate frequency in the receiver 3 and then output to the signal processor 4. The signal processor 4 performs a suppression process on a received signal other than the target signal, determines a signal having a certain level or higher from the received signal as a reflected signal from the target signal, and outputs the signal to the amplitude comparator 5 and the storage device 7. . As shown in FIG. 5B, the storage unit 7 stores a target signal in an azimuth adjacent beam scanned earlier than the current azimuth.
(Sum video of target signal received by beam one direction ahead)
Is output to the amplitude comparator 5. The amplitude comparator 5 compares the sum video of the target signal of the current azimuth and the target signal of the azimuth adjacent beam scanned in the past, and when the latter is larger,
The signal is output to the monopulse angle calculator 6. The monopulse angle measurement calculator 6 calculates the azimuth of the target signal by monopulse angle measurement processing and outputs it.

【0004】ここで、モノパルス測角処理の原理を図3
及び図4を参照して説明する。和パターン101と差パ
ターン102の2種類のアンテナパターンから目標信号
104として和ビデオと差ビデオが得られる。和ビデオ
と差ビデオの振幅値をそれぞれΣ,Δとすれば、和パタ
ーンのビームノーズからの偏差角θは図4の振幅特性曲
線より求められる。この偏差角θとビーム方向を加算す
ることにより、目標の方位角が得られる。
Here, the principle of the monopulse angle measurement processing is shown in FIG.
This will be described with reference to FIG. A sum video and a difference video are obtained as a target signal 104 from two types of antenna patterns, a sum pattern 101 and a difference pattern 102. Assuming that the amplitude values of the sum video and the difference video are Σ and Δ, respectively, the deviation angle θ of the sum pattern from the beam nose can be obtained from the amplitude characteristic curve of FIG. By adding the deviation angle θ and the beam direction, a target azimuth can be obtained.

【0005】[0005]

【発明が解決しようとする課題】この従来のレーダ装置
では、方位測角としてモノパルス測角処理を行っている
ために、和パターンのビームノーズ付近に測角精度が劣
化する不感帯が生じる。ここで、不感帯について図3を
参照して説明する。和パターン101において、ビーム
ノーズ付近では受信レベルが高いので、目標信号105
の受信は容易である。ところが、この領域はちょうど差
パターン102のナル点付近に相当しているため、目標
信号105の差ビデオはノイズに埋もれて、正確な振幅
値Δが得られない。このため、図4に示すようにこの領
域は正確な測角値が得られない不感帯201になるとい
う問題点がある。さらに和パターン101のビームノー
ズから離れるに従って、和ビデオのS/Nが劣化するこ
とによる測角精度の劣化という問題点があった。本発明
の目的は、測角精度を改善したレーダ装置を提供するこ
とにある。
In this conventional radar apparatus, since the monopulse angle measurement is performed as the azimuth angle measurement, a dead zone where the angle measurement accuracy is deteriorated occurs near the beam nose of the sum pattern. Here, the dead zone will be described with reference to FIG. In the sum pattern 101, since the reception level is high near the beam nose, the target signal 105
Is easy to receive. However, since this area corresponds to the vicinity of the null point of the difference pattern 102, the difference video of the target signal 105 is buried in noise, and an accurate amplitude value Δ cannot be obtained. For this reason, as shown in FIG. 4, there is a problem that this area becomes a dead zone 201 where an accurate angle measurement value cannot be obtained. Further, as the distance from the beam nose of the sum pattern 101 increases, the S / N ratio of the sum video deteriorates, which causes a problem that the angle measurement accuracy deteriorates. An object of the present invention is to provide a radar device with improved angle measurement accuracy.

【0006】[0006]

【課題を解決するための手段】本発明のレーダ装置は、
ビーム方向制御器、空中線、受信機、信号処理器、モノ
パルス測角演算器、記憶器、及び振幅比較器を有するレ
ーダ装置に、方位方向に隣接する2ビームの和ビデオの
振幅を比較・内挿計算することにより目標の方位角を算
出する振幅比較測角演算器と、モノパルス測角演算器出
力の方位角を入力とし、前記和パターンのノーズ付近及
び前記隣接する2ビームの中間付近では前記振幅比較測
角演算器の出力に重みを掛け、その2つの領域の領域の
中間領域では前記モノパルス測角演算器の出力に重みを
掛けるような重み付け係数を発生させる重み付け係数発
生器と、前記重み付け係数発生器で発生された重み付け
係数に基づいて前記モノパルス測角演算器出力の方位角
前記振幅比較測角演算器出力の方位角との重み付け平
均計算を行う重み付け平均値算出器とを備える。
The radar apparatus according to the present invention comprises:
Compare and interpolate the sum video amplitude of two beams adjacent in the azimuth direction to a radar device that has a beam direction controller, antenna, receiver, signal processor, monopulse goniometer, memory, and amplitude comparator. An amplitude comparison goniometer that calculates the target azimuth by calculating, and an azimuth of the output of the monopulse goniometer, are used as inputs, and the vicinity of the nose of the sum pattern and
And the amplitude comparison measurement near the middle of the two adjacent beams.
The output of the angle calculator is weighted, and the two
In the middle area, the output of the monopulse angle measurement calculator is weighted.
A weighting coefficient generator for generating a weighting coefficient as multiplied, the generated weighted by the weighting coefficient generator
A weighted average value calculator for performing a weighted average calculation of the azimuth angle of the output of the monopulse angle measurement unit and the azimuth angle of the output of the amplitude comparison angle measurement unit based on the coefficient .

【0007】[0007]

【作用】図5(c)に示すように、和パターンのビーム
ノーズ付近及び隣接2ビームの中間付近では振幅比較測
角演算器の出力に重みを掛け、その2つの領域の中間で
は逆にモノパルス測角演算器の出力に重みを掛けるよう
に重み付け係数を設定し、この係数をモノパルス測角演
算器の出力及び振幅比較測角演算器の出力とともに重み
付け平均値算出器で重み付け平均計算を行ない、目標の
方位角として出力する。
As shown in FIG . 5 (c), the output of the amplitude comparison and angle measurement calculator is weighted in the vicinity of the beam nose of the sum pattern and in the vicinity of the middle of two adjacent beams. A weighting coefficient is set so as to weight the output of the angle measurement arithmetic unit, and the weighted average calculation is performed by a weighted average value calculator together with the output of the monopulse angle measurement arithmetic unit and the output of the amplitude comparison angle measurement arithmetic unit. Output as the target azimuth.

【0008】[0008]

【実施例】次に、本発明について図面を参照して説明す
る。図1は本発明の一実施例を示すブロック図である。
尚、図2に示した従来技術の構成と同一部分には同一の
符号を付してあり、ビーム制御器1、空中線2、受信機
3、信号処理器4、振幅比較器5、モノパルス測角演算
器6、記憶器7の動作は従来技術と同様であるため説明
を省略する。本発明では、この構成に更に振幅比較測角
演算器8、重み付け係数発生器9、重み付け平均値算出
器を付設している。前記振幅比較測角演算器8は、信号
処理器4出力の現在の方位の目標信号の和ビデオの振幅
値と、記憶器7出力の方位方向に隣接するビームの目標
信号の和ビデオの振幅値を比較・内挿計算することによ
り、目標の方位角を算出し、出力する。又、重み付け係
数発生器9は、モノパルス測角演算器6出力の目標の方
位角を入力パラメータとして重み付け係数を発生させ
る。
Next, the present invention will be described with reference to the drawings. FIG. 1 is a block diagram showing one embodiment of the present invention.
The same parts as those of the prior art shown in FIG. 2 are denoted by the same reference numerals, and are denoted by a beam controller 1, an antenna 2, a receiver 3, a signal processor 4, an amplitude comparator 5, a monopulse angle measuring device. The operations of the arithmetic unit 6 and the storage unit 7 are the same as those in the related art, and thus the description is omitted. In the present invention, an amplitude comparison angle measurement calculator 8, a weighting coefficient generator 9, and a weighted average value calculator are further provided in this configuration. The amplitude comparison and angle calculation unit 8 calculates the sum video amplitude value of the target signal of the current azimuth output from the signal processor 4 and the sum video amplitude value of the target signal of the beam adjacent in the azimuth direction of the storage unit 7 output. Is calculated and interpolated to calculate the azimuth angle of the target, which is output. The weighting coefficient generator 9 generates a weighting coefficient by using the target azimuth output from the monopulse angle measurement calculator 6 as an input parameter.

【0009】重み付け係数の決め方は次のようにする。
先ず、振幅比較測角演算器8の出力の方位角は、目標の
フラクチュエーション(目標の形や電波伝搬上の性質に
よって生じる時間的振幅変動)による誤差が大きい代わ
りに、モノパルス測角のような不感帯はなく、方位に関
して精度は一様であると見てよい。逆に、モノパルス測
角演算器6の出力の方位角は、目標のフラクチュエーシ
ョンによる誤差がない代わりに、不感帯が生じるととも
に、和パターンのビームノーズから離れた領域ではS/
Nの劣化により測角精度が劣化している。
The method of determining the weighting coefficient is as follows.
First, the azimuth angle of the output of the amplitude comparison angle measurement calculator 8 is determined by the target fraction ( depending on the shape of the target and the properties in radio wave propagation).
Instead of a large error due to temporal amplitude fluctuations , there is no dead zone as in monopulse angle measurement, and it can be seen that the accuracy is uniform with respect to azimuth. Conversely, the azimuth angle of the output of the monopulse angle measuring unit 6 has no error due to the target fractionation, but has a dead zone and S / S in a region apart from the beam nose of the sum pattern.
Angle measurement accuracy is deteriorated due to deterioration of N.

【0010】したがって、重み付け係数としては、和パ
ターンのビームノーズ付近及び隣接2ビームの中間付近
では振幅比較測角演算器8の出力に重みを掛け、その2
つの領域の中間では逆にモノパルス測角演算器6の出力
に重みが掛かるように、重み付け係数を設定する。この
ようにして定めた重み付け係数は、モノパルス測角演算
器6の出力及び振幅比較測角演算器8の出力とともに重
み付け平均値算出器10に入力され、重み付け平均計算
を行った後に、目標の方位角として出力される。
Therefore, as the weighting coefficient, the output of the amplitude comparison and angle measurement calculator 8 is weighted near the beam nose of the sum pattern and near the middle of two adjacent beams.
In the middle of the two areas, a weighting coefficient is set so that the output of the monopulse angle measuring unit 6 is weighted conversely. The weighting coefficient determined in this way is input to the weighted average value calculator 10 together with the output of the monopulse angle measurement arithmetic unit 6 and the output of the amplitude comparison angle measurement arithmetic unit 8, and after performing the weighted average calculation, the target azimuth is calculated. Output as corners.

【0011】[0011]

【発明の効果】以上説明したように本発明は、方位測角
において、モノパルス測角処理を行うとともに、方位隣
接2ビーム和ビデオを用いて振幅比較測角処理を行
い、両方の出力に対してモノパルス測角における不感帯
の誤差と和パターンのビームノーズより離れた領域での
S/N劣化による誤差及び振幅比較測角における目標の
フラクチュエーションの誤差を考慮した重み付け平均計
算を行うことにより、測角精度を改善するという効果が
ある。
As described above, according to the present invention, in the azimuth angle measurement, the monopulse angle measurement process is performed, and the amplitude comparison angle measurement process is performed using the sum video of the two beams adjacent to the direction. The weighted average calculation takes into account the error in the dead band in the monopulse angle measurement, the error due to S / N deterioration in the area apart from the beam nose of the sum pattern, and the error in the target fractionation in the amplitude comparison angle measurement. This has the effect of improving angular accuracy.

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

【図1】本発明のレーダ装置の一実施例のブロック構成
図である。
FIG. 1 is a block diagram showing an embodiment of a radar apparatus according to the present invention.

【図2】従来のレーダ装置の一例のブロック構成図であ
る。
FIG. 2 is a block diagram illustrating an example of a conventional radar apparatus.

【図3】モノパルス測角方式におけるビームパターンの
概念図である。
FIG. 3 is a conceptual diagram of a beam pattern in a monopulse angle measurement method.

【図4】モノパルス測角方式における振幅特性曲線であ
る。
FIG. 4 is an amplitude characteristic curve in a monopulse angle measurement method.

【図5】本発明における方位隣接ビームを説明するため
の図である。
FIG. 5 is a diagram for explaining azimuth adjacent beams in the present invention.

【符号の説明】[Explanation of symbols]

1 ビーム方向制御器 2 空中線 3 受信機 4 信号処理器 5 振幅比較器 6 モノパルス測角演算器 7 記憶器 8 振幅比較測角演算器 9 重み付け係数発生器 10 重み付け平均値算出器 DESCRIPTION OF SYMBOLS 1 Beam direction controller 2 Antenna 3 Receiver 4 Signal processor 5 Amplitude comparator 6 Monopulse angle measuring unit 7 Storage unit 8 Amplitude comparison angle measuring unit 9 Weighting coefficient generator 10 Weighted average value calculator

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 所定のビーム走査プログラムに従ってビ
ーム方向を制御するビーム方向制御器と、前記ビーム方
向制御器により定められたビーム方向において方位方向
にモノパルス測角用の和パターンと差パターンを同時に
形成することが可能な空中線と、前記空中線を通して
号を受信する受信機と、目標信号以外の受信信号を抑圧
する信号処理器と、前記和パターンと差パターンの振幅
特性により目標の方位角を算出するモノパルス測角演算
器と、前記信号処理器からの信号処理出力の目標信号を
記憶する記憶器と、方位方向に隣接する2ビームの和ビ
デオの振幅を比較する振幅比較器と、方位方向に隣接す
る2ビームの和ビデオの振幅を比較・内挿計算すること
により目標の方位角を算出する振幅比較測角演算器と、
モノパルス測角演算器出力の方位角を入力とし、前記和
パターンのノーズ付近及び前記隣接する2ビームの中間
付近では前記振幅比較測角演算器の出力に重みを掛け、
その2つの領域の領域の中間領域では前記モノパルス測
角演算器の出力に重みを掛けるような重み付け係数を発
生させる重み付け係数発生器と、前記重み付け係数発生
器で発生された重み付け係数に基づいて前記モノパルス
測角演算器出力の方位角と前記振幅比較測角演算器出力
の方位角との重み付け平均計算を行う重み付け平均値算
出器とを備えることを特徴とするレーダ装置。
1. A and the beam direction controller for controlling the beam direction in accordance with a predetermined beam scanning program, said beam direction
An antenna capable of simultaneously forming a sum pattern and a difference pattern for monopulse angle measurement in the azimuth direction in the beam direction determined by the direction controller, and a receiver for receiving a signal through the antenna , a signal processor for suppressing the received signal other than the target signal, the monopulse angle measuring calculator for calculating the azimuth angle of the target by the amplitude characteristic of the sum pattern and difference pattern, the target signal of the signal processing output from the signal processor And an amplitude comparator for comparing the amplitude of the sum video of two beams adjacent in the azimuth direction, and comparing and interpolating the amplitude of the sum video of two beams adjacent in the azimuth direction to calculate the target. An amplitude comparison angle measurement calculator for calculating an azimuth angle,
The azimuth of the output of the monopulse angle measurement unit is input and the sum
Near the nose of the pattern and between the two adjacent beams
In the vicinity, weighting is applied to the output of the amplitude comparison angle measurement calculator,
In the middle area between the two areas, the monopulse measurement is performed.
A weighting coefficient generator for generating a weighting coefficient that multiplies the weight to output angular calculator, the weighting coefficient generating
Characterized in that on the basis of the generated weighting coefficients vessel and a weighted average calculator to perform a weighted average calculation of the azimuth angle of said amplitude comparison angle measuring operation output and the azimuth angle of the monopulse angle measuring operation output Radar equipment.
JP34236491A 1991-11-30 1991-11-30 Radar equipment Expired - Lifetime JP2699740B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP34236491A JP2699740B2 (en) 1991-11-30 1991-11-30 Radar equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP34236491A JP2699740B2 (en) 1991-11-30 1991-11-30 Radar equipment

Publications (2)

Publication Number Publication Date
JPH05150036A JPH05150036A (en) 1993-06-18
JP2699740B2 true JP2699740B2 (en) 1998-01-19

Family

ID=18353157

Family Applications (1)

Application Number Title Priority Date Filing Date
JP34236491A Expired - Lifetime JP2699740B2 (en) 1991-11-30 1991-11-30 Radar equipment

Country Status (1)

Country Link
JP (1) JP2699740B2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01293497A (en) * 1988-05-21 1989-11-27 Fuji Electric Co Ltd Automatic rental machine
JP2591482B2 (en) * 1994-06-10 1997-03-19 日本電気株式会社 Target detection circuit
JP4368852B2 (en) 2003-09-11 2009-11-18 三菱電機株式会社 Radar equipment
CN108169740B (en) * 2017-12-27 2019-12-20 中国电子科技集团公司第五十四研究所 Angle measuring method for radar sequential lobe amplitude comparison

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