JPH07101232B2 - Multi-target tracking method and apparatus - Google Patents

Multi-target tracking method and apparatus

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Publication number
JPH07101232B2
JPH07101232B2 JP2232556A JP23255690A JPH07101232B2 JP H07101232 B2 JPH07101232 B2 JP H07101232B2 JP 2232556 A JP2232556 A JP 2232556A JP 23255690 A JP23255690 A JP 23255690A JP H07101232 B2 JPH07101232 B2 JP H07101232B2
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Prior art keywords
target
hypothesis
data
detection data
tracking
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JPH04113291A (en
Inventor
雅迪 関根
達也 鈴木
義夫 小菅
尚雄 岩間
敏樹 饗場
博道 川添
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防衛庁技術研究本部長
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Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は探知データが新目標か既追尾目標かクラツタ
等の不要信号かという航跡の仮説を生成し,その仮説の
信頼度を基にクラツタ等の不要信号を除去しながら多目
標を追尾する多目標追尾方法及びその装置に関するもの
である。
DETAILED DESCRIPTION OF THE INVENTION [Industrial field of application] This invention generates a track hypothesis indicating whether the detection data is a new target, a tracked target, or an unnecessary signal such as a clutter, and based on the reliability of the hypothesis, the clutter The present invention relates to a multi-target tracking method and apparatus for tracking multi-targets while removing unnecessary signals such as.

〔従来の技術〕[Conventional technology]

従来の方法は,第3図に示すように目標の位置及び探知
時刻等の探知データを入力し(ステツプ12),この探知
データ(探知時刻)及び各目標の平滑諸元を基に各目標
の予測諸元を計算し(ステツプ13),探知データを極座
標から直交座標に変換し(ステツプ14),上記予測諸元
を基に各目標のソフトウエアゲート(次以降の探知時刻
での目標の予測存在範囲)を計算し(ステツプ16),上
記探知データ及び上記ソフトウエアゲートを基にクラス
タを生成し(ステツプ17),上記クラスタの生成結果を
基に上記探知データが新目標か既追尾目標かクラツタ等
の不要信号かという航跡の仮説を生成し(ステツプ1
8),この仮説及び上記探知データを基にその信頼度を
計算すると共にクラツタ等の不要信号を除去し(ステツ
プ19),このクラツタ等の不要信号を除去した後の仮説
信頼度,上記探知データ及び上記予測諸元を基に各目標
の平滑諸元を計算し(ステツプ20),上記仮説の信頼度
により追尾が確立したかを判断し(ステツプ21),追尾
が確立した時,上記平滑諸元を出力し(ステツプ22),
終了か否かを判断し(ステツプ23),終了でない時,ま
た,初めから繰り返すようになつていた。
The conventional method inputs detection data such as the position and detection time of the target as shown in FIG. 3 (step 12), and based on this detection data (detection time) and smoothing specifications of each target, Prediction parameters are calculated (step 13), the detection data is converted from polar coordinates to Cartesian coordinates (step 14), and the software gate of each target (target prediction at the next and subsequent detection times) is calculated based on the above prediction parameters. Existence range) is calculated (step 16), a cluster is generated based on the detection data and the software gate (step 17), and whether the detection data is a new target or a tracked target based on the generation result of the cluster. A hypothesis of a wake such as an unwanted signal such as clutter is generated (Step 1
8) Calculate the reliability based on this hypothesis and the above detection data, and remove unnecessary signals such as clutter (step 19), and the hypothesis reliability after removing unnecessary signals such as this clutter and the above detection data. Then, the smoothing parameters of each target are calculated based on the above prediction parameters (step 20), and it is judged from the reliability of the above hypothesis whether tracking has been established (step 21). Output the original (step 22),
It was judged whether or not it was finished (step 23), and when it was not finished, it was repeated from the beginning.

従来の装置は,第4図に示すように,レーダビデオを受
信するフエイズドアレイアンテナ(1)と,このフエイ
ズドアレイアンテナ(1)から得られるレーダビデオを
レーダ信号処理するレーダ信号処理装置(2)と,この
レーダ信号処理装置(2)から算出される極座標系での
探知データを直交座標に変換する座標変換装置(4)
と,上記座標変換装置(4)から算出される探知データ
及び各目標の平滑諸元を基に各目標の予測諸元を計算す
る目標予測処理装置(3)と,この目標予測処理装置
(3)から算出される予測諸元を基に各目標のソフトウ
エアゲート(次以降の探知時刻での目標の予測存在範
囲)を計算するソフトウエアゲート算出装置(8)と,
このソフトウエアゲート算出装置(8)から算出される
ソフトウエアゲート及び上記座標変換装置(4)から算
出される探知データを基にクラスタを生成するクラスタ
生成装置(9)と,このクラスタ生成装置(9)から得
られるクラスタ生成結果を基に上記座標変換装置(4)
から算出される検知データが新目標か既追尾目標かクラ
ツタ等の不要信号かという航跡の仮説を生成する航跡仮
説生成装置(10)と,この航跡仮説生成装置(10)から
得られる仮説及び上記探知データを基にその信頼度を計
算すると共にクラツタ等の不要信号を除去する仮説信頼
度算出装置(11)と,この仮説信頼度算出装置(11)か
ら算出されるクラツタ等の不要信号を除去した後の仮説
信頼度,上記探知データ及び上記目標予測処理装置
(3)から算出される予測諸元を基に各目標の平滑諸元
を計算する目標平滑処理装置(12)と,上記仮説信頼度
により追尾が確立したかを判断する追尾確立判定装置
(13)と,この追尾確立判定装置(13)に繋がる航跡を
表示する航跡表示装置(14)からなつていた。
As shown in FIG. 4, the conventional device is a phased array antenna (1) for receiving a radar video and a radar signal processing for processing a radar video obtained from the phased array antenna (1) as a radar signal. A device (2) and a coordinate conversion device (4) for converting detection data in a polar coordinate system calculated from the radar signal processing device (2) into rectangular coordinates.
And a target prediction processing device (3) for calculating prediction data of each target based on the detection data calculated from the coordinate conversion device (4) and smooth data of each target, and the target prediction processing device (3). ), A software gate calculation device (8) for calculating a software gate of each target (predicted existence range of the target at the next detection time) based on the prediction specifications calculated from
A cluster generation device (9) for generating a cluster based on the software gate calculated by the software gate calculation device (8) and the detection data calculated by the coordinate conversion device (4), and this cluster generation device ( The coordinate conversion device (4) based on the cluster generation result obtained from 9).
A track hypothesis generator (10) that generates a track hypothesis that the detection data calculated from is a new target, an already-tracked target, or an unnecessary signal such as clutter, and a hypothesis obtained from this track hypothesis generator (10) and the above A hypothesis reliability calculation device (11) that calculates the reliability based on detection data and removes unnecessary signals such as clutter, and removes unnecessary signals such as clutter calculated from this hypothesis reliability calculation device (11) Target smoothing device (12) for calculating smoothing parameters of each target based on the reliability of the hypothesis, the detection data, and the prediction parameters calculated from the target prediction processing device (3); The tracking establishment determination device (13) determines whether tracking has been established according to the degree, and the track display device (14) that displays the track connected to this tracking establishment determination device (13).

〔発明が解決しようとする課題〕[Problems to be Solved by the Invention]

従来の第3図,及び第4図に示すような多目標追尾方法
及びその装置では,入力されてくる探知データをいつで
も座標変換装置により処理を加えていたため,入力され
てくる探知データの数が多い場合,座標変換処理に時間
がかかり過ぎてしまいリアルタイムでは処理しきれな
い。特に追尾開始時には目標の予測存在範囲が確実に定
まらないため,多数の探知データが入力されてくる可能
性が大きい。その結果,多目標の追尾開始時における性
能が極めて悪かつた。
In the conventional multi-target tracking method and apparatus as shown in FIG. 3 and FIG. 4, since the input transform data is always processed by the coordinate transformation device, the number of the sense data input is small. If there are many, the coordinate conversion process takes too much time and cannot be processed in real time. In particular, since the predicted existence range of the target is not definitely determined at the start of tracking, there is a high possibility that many detection data will be input. As a result, the performance at the start of tracking multiple targets was extremely poor.

この発明は,かかる課題を解決するためになされたもの
であり,追尾開始時における処理時間を短縮して多目標
追尾能力を向上させることを目的とする。
The present invention has been made to solve such a problem, and an object thereof is to shorten the processing time at the start of tracking and improve the multi-target tracking capability.

〔課題を解決するための手段〕[Means for Solving the Problems]

この発明に係わる多目標追尾方法及びその装置は,追尾
開始時における処理時間短縮のために,座標系選択装置
を設けたものである。
The multi-target tracking method and apparatus according to the present invention are provided with a coordinate system selection device in order to shorten the processing time at the start of tracking.

〔作用〕[Action]

この発明においては,追尾開始処理時,最初の数回の動
作については座標変換を行わず,観測諸元である極座標
系のままで高速で処理させることを図り,安定な動作と
なつてから目標諸元の正確な算出のできる直交座標系に
切り替えるようにし,その結果として追尾を確立するの
に要する時間を短縮し多目標追尾能力を向上させること
ができる。
In the present invention, during tracking start processing, coordinate conversion is not performed for the first few operations, and high-speed processing is performed in the polar coordinate system, which is the specification of the observation. By switching to a Cartesian coordinate system that enables accurate calculation of specifications, it is possible to shorten the time required to establish tracking and improve multi-target tracking capability.

〔実施例〕〔Example〕

第1図はこの発明の一実施例を示す多目標追尾装置のブ
ロツク図であり,第1図において(1)〜(4),
(8)〜(14)は第4図に示したものと同じである。
(5)は目標予測処理装置(3)から極座標系で出力さ
れた各目標の予測諸元を北基準直交座標に変換する座標
変換装置,(6)はレーダ信号処理装置(2)及び目標
予測処理装置(3)から入力される各目標の探知位置及
び予測諸元の座標系を選択する,座標系選択装置,
(7)は,座標系選択装置(6)において選択を行う際
の判断基準を定めるデータを,前もつて格納する選択デ
ータテーブルである。
FIG. 1 is a block diagram of a multi-target tracking device showing one embodiment of the present invention. In FIG. 1, (1) to (4),
(8) to (14) are the same as those shown in FIG.
(5) is a coordinate conversion device that converts the prediction data of each target output from the target prediction processing device (3) in the polar coordinate system into north reference Cartesian coordinates, and (6) is the radar signal processing device (2) and target prediction A coordinate system selecting device for selecting the coordinate system of each target detection position and prediction data input from the processing device (3),
(7) is a selection data table that stores in advance the data that defines the judgment criteria when making a selection in the coordinate system selection device (6).

第2図はこの発明による多目標追尾方法の一実施例の処
理手順を示す図である。第2図においてフエイズドアレ
イアンテナ(1)から得られたレーダビデオデータをレ
ーダ信号処理するレーダ信号処理装置(2)から位置,
探知時刻等の探知データを入力し(ステツプ12),目標
予測処理装置(3)でこの探知データ(探知時刻)及び
各目標の平滑諸元を基に各目標の予測諸元を計算し(ス
テツプ13),第1の座標変換装置(4)および第2の座
標変換装置(5)で極座標系から直交座標系に変換し
(ステツプ14),座標系選択装置(6)で上記2つの座
標系のうちどちらかを選択し(ステツプ15),ソフトウ
エアゲート算出装置(8)で上記予測諸元を基に各目標
のソフトウエアゲート(次以降の探知時刻での目標の予
測存在範囲)を計算し(ステツプ16),クラスタ生成装
置(9)で上記探知データ,上記初期ソフトウエアゲー
ト及び上記ソフトウエアゲートを基にクラスタを生成し
(ステツプ17),航跡仮説生成装置(10)で上記クラス
タの生成結果を基に上記探知データが新目標が既追尾目
標かクラツタ等の不要信号かという航跡の仮説を生成し
(ステツプ18),仮説信頼度算出装置(11)でこの仮説
及び上記探知データを基に仮説の信頼度を計算すると共
にクラツタ等の不要信号を除去し(ステツプ19),目標
平滑処理装置(12)でこのクラツタ等の不要信号を除去
した後の仮説信頼度,上記探知データ及び上記予測諸元
を基に各目標の平滑諸元を計算し(ステツプ20),追尾
確立判定装置(13)で上記仮説の信頼度により追尾が確
立したかを判断し(ステツプ21),追尾が確立した時,
上記平滑諸元を航跡表示装置(14)へ出力し(ステツプ
22),終了か否かを判断し(ステツプ23),終了でない
時,また,初めから繰り返す。
FIG. 2 is a diagram showing a processing procedure of an embodiment of the multi-target tracking method according to the present invention. In FIG. 2, the position of a radar signal processing device (2) for processing radar video data obtained from the phased array antenna (1) from the radar signal processing device (2),
The detection data such as the detection time is input (step 12), and the target prediction processing unit (3) calculates the prediction parameters of each target based on the detection data (detection time) and the smooth parameters of each target (step 12). 13), the first coordinate conversion device (4) and the second coordinate conversion device (5) convert from the polar coordinate system to the orthogonal coordinate system (step 14), and the coordinate system selection device (6) converts the two coordinate systems Either of them is selected (step 15), and the software gate calculation device (8) calculates the software gate of each target (predicted existence range of the target at the detection time after that) based on the above-mentioned prediction specifications. (Step 16), the cluster generator (9) generates a cluster based on the detection data, the initial software gate and the software gate (step 17), and the track hypothesis generator (10) generates the cluster. Based on the generated result The intelligent data generates a track hypothesis as to whether the new target is an already tracked target or an unnecessary signal such as clutter (step 18), and the hypothesis reliability calculation device (11) uses this hypothesis and the above detection data to determine the reliability of the hypothesis. Is calculated and unnecessary signals such as clutter are removed (step 19), and the hypothesis reliability after the unnecessary signals such as clutter are removed by the target smoothing processor (12), the detection data, and the above-mentioned prediction parameters are calculated. Then, the smoothing parameters of each target are calculated (step 20), and the tracking establishment determination device (13) judges whether or not the tracking is established based on the reliability of the above hypothesis (step 21). When the tracking is established,
The above smoothed parameters are output to the track display device (14) (step
22), it is judged whether or not it is finished (step 23), and when it is not finished, it is repeated from the beginning.

上記の処理を以下に具体的に説明する。The above processing will be specifically described below.

目標予測処理装置(3)は,(1)式により各目標の予
測諸元を算出する。
The target prediction processing device (3) calculates the prediction specifications of each target by the formula (1).

ここでX k m(−)は予測諸元ベクトル Φk-1は推移行列X k m(+)は平滑諸元ベクトル Kは時刻tk mは既追尾目標番号 Pkm(−)は予測諸元(誤差共分散行列) Pk-1m(+)は平滑諸元(誤差共分散行列) Γ1(k-1)はプロセス雑音変換行列 Qk-1はカルマンフイルタにおけるプロセス雑音 (目標運動のゆらぎの成分) Tは転置行列の意味を示す。 Here X k m (-) prediction specifications vector Φ k-1 is the transition matrix X k m (+) is smooth specifications vector K is time t k m is already tracking the target number P k m (-) prediction Parameters (error covariance matrix) P k-1 m (+) is smooth parameter (error covariance matrix) Γ 1 (k-1) is process noise conversion matrix Q k-1 is process noise in Kalman filter (target Motion fluctuation component) T represents the meaning of a transposed matrix.

第1の座標変換装置(4)および第2の座標変換装置
(5)における座標変換の方法は以下のとおりである。
The method of coordinate conversion in the first coordinate conversion device (4) and the second coordinate conversion device (5) is as follows.

座標系選択装置(6)での判断の基準は,追尾動作の回
数(3回目で切り替え等)で定めることができる。その
動作例を表1に示す。
The criterion for the determination by the coordinate system selection device (6) can be determined by the number of tracking operations (switching at the third time, etc.). Table 1 shows an example of the operation.

ソフトウエアゲート算出装置(8)におけるソフトウエ
アゲート算出方法を以下に示す。
The software gate calculation method in the software gate calculation device (8) is shown below.

ここでZ k (−)mはソフトウエアゲートの中心位置ベクトル Hkは観測変換行列 Sk,mはソフトウエアゲートの広がりを示す行列 Γ2(k)は観測雑音変換行列 Rkは観測雑音共分散行列 クラスタ生成装置(9)におけるクラスタ生成条件およ
び算出方法を示す。
Where Z k (−) m is the center position vector of the software gate H k is the observation transformation matrix S k, m is the matrix showing the spread of the software gate Γ 2 (k) is the observation noise transformation matrix R k is the observation noise The covariance matrix cluster generation device (9) shows a cluster generation condition and a calculation method.

ここでZ kは探知位置ベクトル Z k(−)lは既追尾目標lの予測位置ベクトル Z k(−)mは既追尾目標mの予測位置ベクトル dは判定しきい値である。 Here, Z k is the detection position vector Z k (−) l is the predicted position vector Z k (−) m of the tracked target l, and the predicted position vector d of the tracked target m is d.

上記のように,探知データZkが既追尾目標lおよびmの
ソフトウエアゲートのどちらにもあてはまる場合はSk,m
とSk,lを統合し,クラスタを生成する。
As described above, when the detection data Z k applies to both the software gates of the already tracked targets l and m, S k, m
And S k, l are integrated to generate a cluster.

Sk′=Sk,m+Sk,l ……(5) ここでSk′がクラスタの広がりを示す行列である。S k ′ = S k, m + S k, l (5) Here, S k ′ is a matrix showing the spread of the cluster.

航跡仮説生成装置(10)における仮説生成方法を示す。A hypothesis generation method in a track hypothesis generation device (10) is shown.

(ア) 探知データの識別 クラツタFZ k,n 既追尾目標Tg 新目標Nh ここでnは探知データ数である。(A) Identification of detection data Clutter F Z k, n Tracked target T g New target N h where n is the number of detection data.

gは既追尾目標数である。g is the already-tracked target number.

hは新目標数である。h is the new target number.

探知データは上記3つのいずれかに識別される。この識
別結果を仮説Xkとする。
The detection data is identified by any of the above three. The result of this discrimination is hypothesis X k .

(イ) 仮説の生成 サンプリング前の仮説Xk-1に最新の探知データの識別結
果を組み合せて,仮説Xkを生成する。仮説は探知データ
の組合せにより複数生成される。
(B) Generation of hypothesis The hypothesis Xk is generated by combining the hypothesis Xk -1 before sampling with the latest detection data identification result. Multiple hypotheses are generated by combining detection data.

Xk={Xk-1}{Xk}={Xk-1}{F,Tg,Nh}……(6) 仮説信頼度算出装置(11)における仮説信頼度の算出方
法を以下に示す。
Xk = { Xk-1 } { Xk } = { Xk-1 } {F, Tg , Nh } ... (6) The calculation method of the hypothesis reliability in the hypothesis reliability calculation device (11) It is shown below.

Pk(i,j)=N(Rp ki−Rokj,BR ki)≧K0 ……(7) ここでP:仮説の信頼度 N(Rp ki−Rokj,SR ki):時刻Tk-1でのi番目の予測位
置と時刻Tkでのj番目の探知位置データとの位置分布 Rp ki=(Rxp ki,Ryp ki,Rzp ki):時刻Tk-1でのi番目
の目標予測位置ベクトル Rokj=(Rxo kj,Ryo kj,Rzo kj):時刻Tkでのj番目の
目標予測位置データベクトル BR kj:時刻Tk-1のi番目のS/Wゲートの広がり N:正規分布確率密度関数 K0:定数 上式が成り立つ時,追尾開始のための探知データの組合
せである仮説Xkを候補として考慮し,時刻tk-1でのi番
目の予測目標と時刻tkでのj番目の探知データとは相関
があり,『航跡』と見なす。
P k (i, j) = N (R p k i−Ro k j, B R k i) ≧ K 0 (7) where P: hypothesis reliability N (R p k i−Ro k j , S R k i): Position distribution between the i-th predicted position at time T k-1 and the j-th detected position data at time T k R p k i = (R xp k i, R yp k i , R zp k i): i-th target predicted position vector at time T k−1 Ro k j = (R xo k j, R yo k j, R zo k j): j-th time at time T k Target predicted position data vector B R k j: Spread of i-th S / W gate at time T k-1 N: Normal distribution probability density function K 0 : Constant When the above equation holds, the detection data for tracking start Considering the combination of the hypothesis X k as a candidate, there is a correlation between the i-th predicted target at time t k−1 and the j-th detection data at time t k , and it is regarded as a “track”.

目標平滑処理装置(12)における平滑値算出方法を以下
に示す。
The smoothing value calculation method in the target smoothing device (12) is shown below.

(ア) 平滑のためのカルマンゲイン算出 Kk,m=Pk(-)mHkSk,m-1 ……(8) ここで,Kk,mはカルマンゲイン (イ) 平滑値算出 ここでX k m (+)は平滑諸元(ベクトル) Pk m(+)は平滑誤差共分散行列である。(A) Kalman gain calculation for smoothing K k, m = P k (-) mH k S k , m -1 (8) where K k, m is Kalman gain (b) Smoothing value calculation Here, X k m (+) is a smoothing parameter (vector) P k m (+) is a smoothing error covariance matrix.

追尾確立判定装置(13)における追尾確立判定方法につ
いて示す。
A tracking establishment determination method in the tracking establishment determination device (13) will be described.

(ア) 全ての仮説の中に,同一の航跡が存在するか調
べる。
(A) Check whether the same track exists in all hypotheses.

(イ) 上記条件を満たした場合,追尾確立とする。(B) When the above conditions are met, tracking is established.

(ウ) 上記条件を満たさない場合,初めからの処理へ
戻る。
(C) If the above conditions are not satisfied, the process returns to the beginning.

また,『追尾が確立した。』とした場合,目標平滑処理
装置(12)から算出される目標平滑諸元を航跡表示装置
(14)へ出力する。
Also, "Tracking has been established. ], The target smoothing specifications calculated from the target smoothing processing device (12) are output to the track display device (14).

〔発明の効果〕〔The invention's effect〕

以上のように,この発明によれば,追尾開始時における
探知データを極座標系のままで処理することにより,多
目標の追尾開始処理を高速に実行でき,その結果として
追尾を確立するのに要する時間を短縮し多目標追尾能力
を向上させることができる。
As described above, according to the present invention, by processing the detection data at the start of tracking in the polar coordinate system as it is, the tracking start processing of multiple targets can be executed at high speed, and as a result, it is necessary to establish the tracking. It is possible to shorten the time and improve the multi-target tracking ability.

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

第1図は,この発明による多目標追尾装置の一実施例の
全体構成図,第2図は,この発明による多目標追尾方法
の一実施例の処理手順を示す図,第3図は,従来の多目
標追尾装置の一実施例の全体構成図,第4図は,従来の
多目標追尾方法の一実施例の処理手順を示す図である。 図において,(1)はフエイズドアレイアンテナ,
(2)はレーダ信号処理装置,(3)は目標予測処理装
置,(4)は第1の座標変換装置,(5)は第2の座標
変換装置,(6)は座標系選択装置,(7)は選択デー
タテーブル,(8)はソフトウエアゲート算出装置,
(9)はクラスタ生成装置,(10)は航跡仮説生成装
置,(11)は仮説信頼度算出装置,(12)は目標平滑処
理装置,(13)は追尾確立判定装置,(14)は航跡表示
装置である。 なお,図中,同一符号は同一または相当部分を示す。
FIG. 1 is an overall configuration diagram of an embodiment of a multi-target tracking device according to the present invention, FIG. 2 is a diagram showing a processing procedure of an embodiment of a multi-target tracking method according to the present invention, and FIG. FIG. 4 is an overall configuration diagram of an embodiment of the multi-target tracking device of FIG. 4, and FIG. 4 is a diagram showing a processing procedure of an embodiment of a conventional multi-target tracking method. In the figure, (1) is a phased array antenna,
(2) is a radar signal processing device, (3) is a target prediction processing device, (4) is a first coordinate conversion device, (5) is a second coordinate conversion device, (6) is a coordinate system selection device, ( 7) is a selection data table, (8) is a software gate calculator,
(9) is a cluster generation device, (10) is a track hypothesis generation device, (11) is a hypothesis reliability calculation device, (12) is a target smoothing device, (13) is a tracking establishment determination device, and (14) is a track It is a display device. In the drawings, the same reference numerals indicate the same or corresponding parts.

フロントページの続き (72)発明者 川添 博道 神奈川県鎌倉市上町屋325番地 三菱電機 株式会社鎌倉製作所内 審査官 中村 和男 (56)参考文献 特開 昭61−186877(JP,A)Front page continuation (72) Inventor Hiromichi Kawazoe 325 Kamimachiya, Kamakura City, Kanagawa Mitsubishi Electric Corporation Kamakura Factory Examiner Kazuo Nakamura (56) References JP-A-61-186877 (JP, A)

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】目標及び不要信号等の位置及び探知時刻等
の探知データを入力し,この探知データ及び各目標の平
滑諸元を基に各目標の予測諸元を計算し,探知データの
観測諸元である極座標系から直交座標系に変換し,上記
座標系のどちらかを選択し,上記予測諸元を基に各目標
のソフトウエアゲート(次以降の探知時刻での目標の予
測存在範囲)を計算し,上記探知データ,上記ソフトウ
エアゲートを基にクラスタ(目標予測存在範囲の集合
体)を生成し,上記クラスタの生成結果を基に上記探知
データが新目標か既追尾目標かクラツタ等の不要信号か
という航跡の仮説を生成し,この仮説及び上記探知デー
タを基に仮説の信頼度を計算すると共にクラツタ等の不
要信号を除去し,このクラツタ等の不要信号を除去した
後の仮説信頼度,上記探知データ及び上記予測諸元を基
に各目標の平滑諸元を計算し,上記仮説の信頼度により
追尾が確立したかを判断し,追尾が確立した時,上記平
滑諸元を出力し,終了か否かを判断し,終了でない時,
また,初めから繰り返し上記処理を行うことを特徴とす
る多目標追尾方法。
1. Detecting data such as position of target and unnecessary signal and detection time such as detection time, calculating prediction data of each target based on this detection data and smoothing data of each target, and observing detection data The specifications are converted from the polar coordinate system to the rectangular coordinate system, one of the above coordinate systems is selected, and the software gate of each target (the predicted existence range of the target at the next and later detection times) is selected based on the above prediction specifications. ) Is calculated, a cluster (aggregate of target predicted existence ranges) is generated based on the detection data and the software gate, and based on the generation result of the cluster, the detection data is a new target, a tracked target, or a clutter. A hypothesis of a wake such as an unnecessary signal such as is generated, the reliability of the hypothesis is calculated based on this hypothesis and the above detection data, unnecessary signals such as clutter are removed, and unnecessary signals such as clutter are removed. Hypothesis reliability, above The smoothing parameters of each target are calculated based on the detection data and the above prediction parameters, and it is judged from the reliability of the above hypothesis whether tracking has been established. When tracking has been established, the smoothing parameters are output and the processing ends. If it is not finished,
In addition, a multi-target tracking method characterized by repeatedly performing the above processing from the beginning.
【請求項2】レーダビデオを受信するフエイズドアレイ
アンテナと,このフエイズドアレイアンテナから得られ
るレーダビデオをレーダ信号処理するレーダ信号処理装
置と,このレーダ信号処理装置から算出される探知デー
タ及び各目標の平滑諸元を基に各目標の予測諸元を計算
する目標予測処理装置と,上記探知データの観測諸元で
ある極座標系から直交座標系に変換する第一,第二の座
標変換装置と,上記座標系を選択する座標系選択装置
と,上記座標系選択装置の選択の基準を定めるデータを
格納した選択データテーブルと,上記目標予測処理装置
から算出される予測諸元を基に各目標のソフトウエアゲ
ート(次以降の探知時刻での目標の予測存在範囲)を計
算するソフトウエアゲート算出装置と,このソフトウエ
アゲート算出装置から算出されるソフトウエアゲート及
び上記レーダ信号処理装置から算出される探知データを
基にクラスタを生成するクラスタ生成装置と,上記クラ
スタ生成装置から得られるクラスタ生成結果を基に上記
レーダ信号処理装置から算出される探知データが新目標
か既追尾目標かクラツタ等の不要信号かという航跡の仮
説を生成する航跡仮説生成装置と,この航跡仮説生成装
置から得られる仮説及び上記探知データを基に仮説の信
頼度を計算すると共にクラツタ等の不要信号を除去する
仮説信頼度算出装置と,この仮説信頼度算出装置から算
出されるクラツタ等の不要信号を除去した後の仮説信頼
度,上記探知データ及び上記目標予測処理装置から算出
される予測諸元を基に各目標の平滑諸元を計算する目標
平滑処理装置と,上記仮説信頼度により追尾が確立した
かを判断する追尾確立判定装置と,この追尾確立判定装
置に繋がる航跡を表示する航跡表示装置とを具備したこ
とを特徴とする多目標追尾装置。
2. A phased array antenna for receiving a radar video, a radar signal processor for processing a radar signal obtained from the phased array antenna as a radar signal, and detection data calculated by the radar signal processor. And a target prediction processing device for calculating the prediction data of each target based on the smooth data of each target, and the first and second coordinates for converting the polar coordinate system, which is the observation data of the detection data, into the orthogonal coordinate system. Based on a conversion device, a coordinate system selection device that selects the coordinate system, a selection data table that stores data that defines the selection criteria of the coordinate system selection device, and prediction specifications calculated from the target prediction processing device. And a software gate calculation device that calculates the software gate of each target (predicted existence range of the target at the detection time after that) and this software gate calculation device. A cluster generation device that generates a cluster based on the calculated software gate and the detection data calculated from the radar signal processing device, and a calculation from the radar signal processing device based on the cluster generation result obtained from the cluster generation device A track hypothesis generating device for generating a track hypothesis indicating whether the detected data is a new target, a tracked target, or an unnecessary signal such as a clutter, and a hypothesis obtained from the track hypothesis generating device and the reliability of the hypothesis based on the detection data. Hypothesis reliability calculating device for calculating the degree and removing unnecessary signals such as clutter, and hypothesis reliability after removing unnecessary signals such as clutter calculated from the hypothesis reliability calculating device, the detection data, and the target A target smoothing processor that calculates smoothing specifications of each target based on the prediction specifications calculated from the prediction processor, and the hypothesis reliability And tracking establishment determination device for determining whether the tracking has been established, the multi-target tracking apparatus characterized by comprising a track display device for displaying a track leading to the tracking establishment determination device.
JP2232556A 1990-09-04 1990-09-04 Multi-target tracking method and apparatus Expired - Lifetime JPH07101232B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2232556A JPH07101232B2 (en) 1990-09-04 1990-09-04 Multi-target tracking method and apparatus

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Application Number Priority Date Filing Date Title
JP2232556A JPH07101232B2 (en) 1990-09-04 1990-09-04 Multi-target tracking method and apparatus

Publications (2)

Publication Number Publication Date
JPH04113291A JPH04113291A (en) 1992-04-14
JPH07101232B2 true JPH07101232B2 (en) 1995-11-01

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US5406289A (en) * 1993-05-18 1995-04-11 International Business Machines Corporation Method and system for tracking multiple regional objects
US5959574A (en) * 1993-12-21 1999-09-28 Colorado State University Research Foundation Method and system for tracking multiple regional objects by multi-dimensional relaxation
US5537119A (en) * 1993-12-21 1996-07-16 Colorado State University Research Foundation Method and system for tracking multiple regional objects by multi-dimensional relaxation
JP5193444B2 (en) * 2006-08-11 2013-05-08 株式会社東芝 Tracking device
JP5422727B2 (en) * 2012-12-04 2014-02-19 株式会社東芝 Tracking device
CN115436933B (en) * 2022-09-22 2025-09-19 中国人民解放军海军航空大学 Target association tracking data set construction method based on self-reporting data
CN115718623B (en) * 2022-11-30 2025-09-16 中国电子科技集团公司第二十研究所 Heterogeneous radar trace fusion parallel processing method in dense clutter environment
CN116859380B (en) * 2023-09-05 2023-11-21 长沙隼眼软件科技有限公司 Method and device for measuring target track, electronic equipment and storage medium
CN117111019B (en) * 2023-10-25 2024-01-09 深圳市先创数字技术有限公司 Target tracking and monitoring method and system based on radar detection

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