JPS63184085A - Tracking processor - Google Patents

Tracking processor

Info

Publication number
JPS63184085A
JPS63184085A JP1653987A JP1653987A JPS63184085A JP S63184085 A JPS63184085 A JP S63184085A JP 1653987 A JP1653987 A JP 1653987A JP 1653987 A JP1653987 A JP 1653987A JP S63184085 A JPS63184085 A JP S63184085A
Authority
JP
Japan
Prior art keywords
tracking
target
gates
gate
data
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.)
Pending
Application number
JP1653987A
Other languages
Japanese (ja)
Inventor
Hideo Yamada
英雄 山田
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 JP1653987A priority Critical patent/JPS63184085A/en
Publication of JPS63184085A publication Critical patent/JPS63184085A/en
Pending legal-status Critical Current

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  • Radar Systems Or Details Thereof (AREA)

Abstract

PURPOSE:To improve followability in tracking by having a plurality of tracking gates for every swing acceleration and, moreover, controlling target detecting level for every tracking gate. CONSTITUTION:Data obtained from a radar instrument are inputted to a target tracking unit 3 and a target is detected by a plurality of tracking gates from a target calculator 4 and target detecting level to output target data to a target buffer 5. The gate calculator 4 outputs the tracking gates and tracking data to a gate correlation processor 6 and outputs the tracking gates and target detecting level to the target detector 3. Thus, by having a plurality of tracking gates for defining a range wherein the position correlation of the target and a track resulted from the tracking of the target at every rotational period in accordance with swing acceleration and further setting optimum target detecting level corresponding to a plurality of the tracking gates for each of a plurality of the tracking gates, target detection is facilitated and tracking is continued.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、レーダー装置、特に、目標と航跡との位置の
相関を行なう追尾ゲートを旋回加速度に応じ複数個有し
、さらに追尾ゲート毎の目標検出レベルを制御して追尾
継続する追尾処理装置に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention provides a radar device, in particular, a radar device that has a plurality of tracking gates that correlate the positions of a target and a track according to turning acceleration, and The present invention relates to a tracking processing device that controls a target detection level to continue tracking.

〔従来の技術〕[Conventional technology]

従来この種のレーダー装置は、航跡の予測位置を中心に
単数個の追尾ゲートであり、またこの追尾ゲートのみの
目標検出レベルを制御する追尾処理装置となっていた。
Conventionally, this type of radar device has a single tracking gate centered on the predicted position of the track, and has also been a tracking processing device that controls the target detection level of only this tracking gate.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

上述した従来の追尾処理装置は、単数個の追尾ゲートで
あシ、また目標検出レベルも旋回に応じた適切な制御が
実施されない場合がアシ、追尾不能又は誤追尾を生じる
欠点がある。
The above-mentioned conventional tracking processing device has a drawback that only a single tracking gate is used, and that if the target detection level is not controlled appropriately according to the turning, it may result in reeds, tracking failure, or incorrect tracking.

〔問題点を解決するための手段〕[Means for solving problems]

本発明の追尾処理装置は、航空機等の旋回速度とoG=
nGの旋回加速度(G:重力加速度を示す)によシ追尾
ゲートを算出するゲート算出部と複数個の追尾ゲートに
相関の優先順位を付けて目標と航跡の相関を実施するゲ
ート相関処理部と、目標の検出レベルを制御する目標検
出部を有している。
The tracking processing device of the present invention has the following characteristics: the turning speed of an aircraft, etc., and oG=
A gate calculation unit that calculates a tracking gate based on a turning acceleration of nG (G: indicates gravitational acceleration); and a gate correlation processing unit that prioritizes correlation between a plurality of tracking gates and correlates a target and a track. , has a target detection section that controls the detection level of the target.

〔実施例〕〔Example〕

次に本発明について図面を参照して説明する。 Next, the present invention will be explained with reference to the drawings.

第1図は、本発明の一実施例を示す。FIG. 1 shows one embodiment of the invention.

レーダー装置から得られたデータ(R,、θi)は、目
標検出部:3へ入力される。目標検出部:3は、ゲート
算出部=4からの追尾ゲート(Go−Gn)及び目標検
出レベル(THGo−THGo)によシ目標を検出し、
目標データ(Xi、Yi)を目標バッファ:5に出力す
る。
The data (R,, θi) obtained from the radar device is input to the target detection section 3. The target detection unit: 3 detects the target based on the tracking gate (Go-Gn) and target detection level (THGo-THGo) from the gate calculation unit = 4,
Output the target data (Xi, Yi) to the target buffer:5.

航跡バッファ:2は、航跡データ(X、 i 、 Y、
 i 。
Track buffer: 2 is the track data (X, i, Y,
i.

VX +−1+”’f j−1、Gn)をゲート算出部
:4へ出力し、ゲート算出部=4は、ゲート相関処理部
:6へ追尾ゲート(Go−Gn)、追尾ゲート優先デー
タ(GkTただし0≦に≦n)及び追尾データ(Xpi
VX +-1+"'f j-1, Gn) is output to the gate calculation section 4, and the gate calculation section 4 outputs the tracking gate (Go-Gn) and the tracking gate priority data ( GkT (0≦≦n) and tracking data (Xpi
.

Ypi)を出力し、目標検出部:3へ追尾ゲート(Go
”−Gn)及び目標検出レベル(THGo−THG r
l )を出力する。
Ypi) and outputs the tracking gate (Go) to the target detection unit:3.
”-Gn) and target detection level (THGo-THG r
l ) is output.

ゲート相関処理部:6は、目標バッファ:5からの目標
データ(Xt、Yt)と追尾ゲート(Go”Gn)及び
追尾ゲート優先データ(Gk)よシ相関処理を実施し、
平滑化処理部=7へ相関が採れたデータ(Xpi +Y
pi 、xi 、Yi)及び相関ゲート(GK)を出力
する。
The gate correlation processing unit 6 performs correlation processing on the target data (Xt, Yt) from the target buffer 5, the tracking gate (Go"Gn), and the tracking gate priority data (Gk),
Correlated data (Xpi +Y
pi, xi, Yi) and a correlation gate (GK).

平滑化処理部ニアは、航跡バッファ=2からの出力デー
タ(Xsi−1*YSt−1+■Xl−1+■yi−1
)とゲート相関処理部=6からのデータにより平滑化処
理を実施し、航跡予測部:8へ平滑化データ(Xsi。
The smoothing processing unit near outputs the output data from the track buffer = 2 (Xsi-1*YSt-1+■Xl-1+■yi-1
) and the data from the gate correlation processing unit = 6, and the smoothed data (Xsi.

Ys i * ■xs i + vys i)及び相関
ゲート(G*)を出力する。
Ys i * xs i + vys i) and the correlation gate (G*) are output.

航跡予測処理8は平滑化処理部ニアからのデータにより
、航跡予測処理を実施し、航跡バッファ:2へ平滑化デ
ータ(Xs++Ys++Vxsi+”ysl)+航跡予
測データ(Xp*+t、Ypi+t)及び相関ゲート(
Gk’ )を出力する。
The track prediction processing 8 executes the track prediction process using the data from the smoothing processing unit Near, and sends the smoothed data (Xs++Ys++Vxsi+”ysl) + track prediction data (Xp*+t, Ypi+t) and the correlation gate (
Gk') is output.

タイミング制御部:9は、レーダー装置:1からのタイ
ミングによシ、各部の処理タイミングを制御する。
The timing control section 9 controls the processing timing of each section based on the timing from the radar device 1.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明は、追尾ゲートを旋回加速度
毎に複数個有し、さらにその個々の追尾ゲート毎に目標
検出レベルを制御することによシ、追尾の追随性を向上
できる効果がある。
As explained above, the present invention has the effect of improving tracking performance by having a plurality of tracking gates for each turning acceleration and controlling the target detection level for each tracking gate. .

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

第1図は、本発明の実施例、第2図は、従来装置の例、
第3図は、本発明の装置で実施した場合の例、第4図は
、目標検出レベルの例である。 第1図の符号は、以下の通シである。 1・・・レーダー装置、2・・・航跡バッファ、3・・
・目標検出部、4・・・ゲート算出部、5・・・目標バ
ッファ、6・・・ゲート相関処理部、7・・・平滑化処
理部、8・・・航跡予測部、9・・・タイミング制御部
。 xo<    (,5 Z (コ Xoく
FIG. 1 shows an example of the present invention, FIG. 2 shows an example of a conventional device,
FIG. 3 shows an example of implementation using the apparatus of the present invention, and FIG. 4 shows an example of the target detection level. The reference numerals in FIG. 1 are as follows. 1... Radar device, 2... Track buffer, 3...
- Target detection unit, 4... Gate calculation unit, 5... Target buffer, 6... Gate correlation processing unit, 7... Smoothing processing unit, 8... Track prediction unit, 9... Timing control section. xo< (,5 Z

Claims (1)

【特許請求の範囲】[Claims] 航空機等の目標を追尾する方式において、目標と目標に
対する追尾結果である航跡との位置相関を行なう範囲を
規定する追尾ゲートを旋回加速度に対応してレーダ回転
周期毎に複数個有し、さらにその複数個の追尾ゲートに
対応した最適な目標検出レベルを複数の追尾ゲート毎に
設定することにより、目標検出を容易として追尾を継続
することを特徴とする追尾処理装置。
In a method for tracking targets such as aircraft, a plurality of tracking gates are provided for each radar rotation period in accordance with the turning acceleration, and the tracking gates define the range in which the positional correlation between the target and the track that is the tracking result for the target is performed. A tracking processing device that facilitates target detection and continues tracking by setting an optimal target detection level corresponding to a plurality of tracking gates for each of the plurality of tracking gates.
JP1653987A 1987-01-26 1987-01-26 Tracking processor Pending JPS63184085A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1653987A JPS63184085A (en) 1987-01-26 1987-01-26 Tracking processor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1653987A JPS63184085A (en) 1987-01-26 1987-01-26 Tracking processor

Publications (1)

Publication Number Publication Date
JPS63184085A true JPS63184085A (en) 1988-07-29

Family

ID=11919070

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1653987A Pending JPS63184085A (en) 1987-01-26 1987-01-26 Tracking processor

Country Status (1)

Country Link
JP (1) JPS63184085A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10572875B2 (en) 2000-04-24 2020-02-25 Visa International Service Association Online account authentication service
WO2023073803A1 (en) * 2021-10-26 2023-05-04 株式会社Fuji Detection method and sensor system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53102693A (en) * 1977-02-18 1978-09-07 Toshiba Corp Tracking unit for pulse radar
JPS59180473A (en) * 1983-03-31 1984-10-13 Nec Corp Prediction tracking system
JPS61186877A (en) * 1985-02-15 1986-08-20 Nec Corp Initial acquisition system of radar target

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53102693A (en) * 1977-02-18 1978-09-07 Toshiba Corp Tracking unit for pulse radar
JPS59180473A (en) * 1983-03-31 1984-10-13 Nec Corp Prediction tracking system
JPS61186877A (en) * 1985-02-15 1986-08-20 Nec Corp Initial acquisition system of radar target

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10572875B2 (en) 2000-04-24 2020-02-25 Visa International Service Association Online account authentication service
WO2023073803A1 (en) * 2021-10-26 2023-05-04 株式会社Fuji Detection method and sensor system

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