JPS62119486A - Radar altitude measuring system - Google Patents

Radar altitude measuring system

Info

Publication number
JPS62119486A
JPS62119486A JP25997785A JP25997785A JPS62119486A JP S62119486 A JPS62119486 A JP S62119486A JP 25997785 A JP25997785 A JP 25997785A JP 25997785 A JP25997785 A JP 25997785A JP S62119486 A JPS62119486 A JP S62119486A
Authority
JP
Japan
Prior art keywords
radar
target
altitude
distance
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
JP25997785A
Other languages
Japanese (ja)
Inventor
Masaya Inagaki
稲垣 連也
Toyohiko Kobayashi
豊彦 小林
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 JP25997785A priority Critical patent/JPS62119486A/en
Publication of JPS62119486A publication Critical patent/JPS62119486A/en
Pending legal-status Critical Current

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  • Radar Systems Or Details Thereof (AREA)

Abstract

PURPOSE:To measure the altitude of a target without increasing the size of an antenna by interlocking a plurality of two-dimensional radars and determining the altitude of the target from the distance data of the target from two points and the bearing data of the target from one of the two points. CONSTITUTION:When a two-dimensional radar 2 finds a target aircraft and measures its distance and bearing, the radar 2 transmits the data thus obtained to another radar 1 by a microwave communication apparatus 7 and the radar 1, receiving the data, and emits a beam to the target in synchronism with the radar 2. An altitude calculating filter 5, incorporating the precise distance and bearing data of the target from the position of the radar 1 and the precise distance data of the target from the position of the radar 2, the latter data being received from the radar 2, calculates altitude of the target.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は航空管制レーダにおけるレーダ測高方式に関す
る。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a radar height measurement method in an air traffic control radar.

〔従来の技術〕[Conventional technology]

従来、航空機の高度を測定する方式としては、トランス
ポンダを搭載した航空機が気圧高度計の値を2次レーダ
のモードCで地上に送シ返すものと、“3次元レーダに
て航空機の仰角と距離から高度を計測するものがあった
Conventionally, there are two ways to measure the altitude of an aircraft: an aircraft equipped with a transponder transmits the barometric altimeter values back to the ground using mode C of a secondary radar, and a three-dimensional radar that measures the altitude based on the elevation angle and distance of the aircraft. There was something to measure altitude.

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

上述した従来の技術のうち、2次レーダを用いた方式は
、航空機がトランスポンダを搭載してい々ければならな
いという制約があり、3次元レーダを同いた方式は、距
離と仰角から高度を測定しているために遠距離にて高度
誤差を小さくするにはアンテナを大きくしなくてはなら
ずシステムが大型化するという欠点がある。
Among the conventional technologies mentioned above, the method using secondary radar has the limitation that the aircraft must be equipped with a transponder, and the method using the same three-dimensional radar measures altitude from distance and elevation angle. Therefore, in order to reduce the altitude error over long distances, the antenna must be made larger, resulting in a larger system.

本発明の目的は、このような欠点を除去し、トランスポ
ンダを不要とし、また3次元レーダを用いなくとも高度
を測定できるようにしたレーダ測高方式を提供すること
にある。
SUMMARY OF THE INVENTION An object of the present invention is to provide a radar height measurement method that eliminates such drawbacks, eliminates the need for a transponder, and allows altitude measurement without using a three-dimensional radar.

〔問題点を解決するだめの手段〕[Failure to solve the problem]

本発明の構成は、目標の方位と距離を高精度で測定する
電子走査アンテナを持つ第1の2次元レーダと、目標の
距離を高精度で測定する機械的走査アンテナを持つ複数
の第2の2次元レーダとを備えたレーダシステムのレー
ダ測高方式において、追尾目標の位置によって前記第1
のレーダと対となる前記第2のレーダの組合わせを変え
、これら対となる各レーダによって糎ぼ同時刻に前記目
標の距離と方位をそれぞれ測定し、これら対となる両レ
ーダの2組のデータから幾何学的に目標の高度を測定す
ることを特徴とする。
The configuration of the present invention includes a first two-dimensional radar having an electronic scanning antenna that measures the direction and distance of the target with high precision, and a plurality of second two-dimensional radars having mechanical scanning antennas that measure the distance of the target with high precision. In a radar height measurement method for a radar system equipped with a two-dimensional radar, the first
The distance and direction of the target are measured at almost the same time by each pair of radars, and the distance and direction of the target are measured at almost the same time by each pair of radars. It is characterized by measuring the altitude of the target geometrically from the data.

〔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ブロック図である。レ
ーダ1は目標Pの方位と距離を高精度で測定する電子走
査2次元アンテナを持った2次元レーダ、レーダ2は目
標の距離のみを高精度に測定し機械的回転によシ走査を
行う過2次元アンテナを持った通常の2次元レーダであ
シ、それぞれ送信装置8および受信機3.MTI4.監
視用指示装置6.マイクロ波通信装置7を備え、2次元
レーダ2には高度算出フィルタ5が含まれる。この2次
元レーダ2は、目標の航空機を発見し距離と方位を測定
すると、そのデータをマイクロ波通信装置7によりレー
ダ1に送信し、それを受信したレーダ1は目標に向けて
レーダ2と同期するようにビームを発射する。高度算出
フィルタ5は、レーダ1の位置からの目標の距離と方位
の精密なデータと、レーダ2から受信したレーダ2の位
置からの目標の距離の精密なデータとを入力して、目標
の高度を算出する。
FIG. 1 is a block diagram showing one embodiment of the present invention. Radar 1 is a two-dimensional radar with an electronic scanning two-dimensional antenna that measures the direction and distance of target P with high precision. Radar 2 is a radar radar that measures only the distance to the target with high precision and performs scanning using mechanical rotation. It is a normal two-dimensional radar with a two-dimensional antenna, and has a transmitter 8 and a receiver 3, respectively. MTI4. Monitoring instruction device6. The two-dimensional radar 2 includes a microwave communication device 7 and an altitude calculation filter 5 . When this two-dimensional radar 2 discovers the target aircraft and measures its distance and direction, it transmits the data to the radar 1 using the microwave communication device 7, and the radar 1 that receives it synchronizes with the radar 2 toward the target. Fire a beam as shown below. The altitude calculation filter 5 inputs precise data on the distance and direction of the target from the position of the radar 1 and precise data on the distance of the target from the position of the radar 2 received from the radar 2, and calculates the altitude of the target. Calculate.

次に入力データと目標の高度との定量的な関係を説明す
る。
Next, the quantitative relationship between input data and target altitude will be explained.

第2図は、これらレーダ1.レーダ2の地球上の位置の
各パラメータの関係を示す図である。目標Pの高度りと
、第1のレーダ5t(1)からの目標Pの直距離R81
と、第2のレーダ8 鵞t2)からの目標Pの直距離R
SSとし、レーダSlにおいてレーダSlと目標Pが見
込む方位角0とすると、3つの入力データとの関係は次
式のように示される。
Figure 2 shows these radars 1. FIG. 2 is a diagram showing the relationship between parameters of the position of radar 2 on the earth. Altitude of target P and direct distance R81 of target P from first radar 5t(1)
and the direct distance R of the target P from the second radar 8 (t2)
Assuming that SS is the azimuth angle at which the radar Sl and the target P look at the radar Sl, the relationship with the three input data is expressed as shown in the following equation.

h=r(I A)+ r”(A” 1)+R%1+h’
  ・・11)ただし1 、d stn−; r=−ro(電波の屈折を考慮に入れたr(Hの補正)
h′・・・・・・レーダーとレーダ2のアンテナの高さ
く同一とする)、 ro・・・・・・地球の半径、 d・・・・・・レーダー、レーダ2の間の直距離(レン
ジ)、Po・・・・・・目標から地表面に下した垂直点
、の誤差との間の関係を計算して得られた高度りの精度
に関する等精度線図を第3図に示す。ここではRst 
、 R82の測定誤差を15m1角度θの測定誤差を0
03°とし、レーダSl、S、が相互に関係する等精度
Iw(最大誤差90m(F)、 180m(hlおよび
270mの))を示している。この図から200 Km
離れて設置されたレーダ81.S、の間では最大誤差2
70mρ)の範囲で目標高度を測定できることがわかる
h=r(I A)+r"(A"1)+R%1+h'
...11) However, 1, d stn-; r=-ro (r (correction of H) taking into account the refraction of radio waves)
h'...The antenna heights of radar and radar 2 are the same), ro...radius of the earth, d...direct distance between radar and radar 2 ( Fig. 3 shows an iso-precision diagram regarding the accuracy of height obtained by calculating the relationship between the error of range) and Po...the vertical point lowered from the target to the ground surface. Here Rst
, The measurement error of R82 is 15m1 The measurement error of angle θ is 0
03°, and the radars Sl and S are shown to have equal precision Iw (maximum error of 90 m (F), 180 m (of hl and 270 m)) relative to each other. 200 km from this figure
Radar 81 installed remotely. The maximum error is 2 between S
It can be seen that the target altitude can be measured within a range of 70mρ).

また、目lIPの高度の測定誤差を一定以内に収めるた
めには、電子走査レーダS1の位置に対する目標位置P
によって対となる機械走査2次元レーダS2の位置が適
当に選ばれていなければならないことがわかる。
In addition, in order to keep the measurement error of the altitude of the eye IP within a certain range, the target position P relative to the position of the electronic scanning radar S1 must be
It can be seen that the position of the paired mechanical scanning two-dimensional radar S2 must be appropriately selected.

第4図はレーダS2を目標の位置によって別の位置にあ
るレーダS2′を選択することによシ、測高可能な誤差
範囲270m(至)の領域を広げた例を示す。
FIG. 4 shows an example in which the range of error that can be measured is expanded to 270 m (up to 270 m) by selecting the radar S2' located at a different position depending on the target position.

すなわち、レーダ79./とレーダS!とを組合せるこ
とKよシ、別の領域(点線範囲)の目標を同じ精度りで
測高することができる仁とがわかる。
That is, radar 79. / and Radar S! It can be seen that by combining this, it is possible to measure the height of a target in a different area (dotted line range) with the same accuracy.

〔発明の効果〕 以上説明したように、本発明は、電子走査2次元レーダ
を含む複数の2次元レーダを連動させて、2地点からの
目標の距離データとそのうちの1地点からの目標の方位
データから目標の高度を決定することによル、アンテナ
を大きくすることなく目標の高度を計測でき、またトラ
ンスポンダを搭載していない航空機の高度を計測できる
という効果かある。
[Effects of the Invention] As explained above, the present invention links a plurality of two-dimensional radars including an electronic scanning two-dimensional radar to obtain target distance data from two points and target direction from one of the points. By determining the altitude of the target from the data, the altitude of the target can be measured without increasing the size of the antenna, and the altitude of an aircraft without a transponder can be measured.

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

第1図は本発明の一実施例を示すブロック図。 第2図は第1図の場合の各入力データの幾何学的関係を
示す概念図、第3図は第1図の一対の電子走査レーダと
機械的走査レーダとによシ測高できる等精度線の平面図
、第4図は第1図で2個の機械的走査レーダを配置し九
場合の等精度線の平面図である。 1・・・・・・電子走査2次元レーダ、2・・・・・・
機械的走査2次元レーダ、3・・・・・・受信機、4・
・・・・・MTI。 5・・・・・・高度算出フィルタ、6・・・・・・監視
用指示装置、7・・・・・・マイクロ波通信装置、8・
・・・・・送信装置。 @桃P タフf11贋算エカルγ
FIG. 1 is a block diagram showing one embodiment of the present invention. Figure 2 is a conceptual diagram showing the geometric relationship of each input data in the case of Figure 1, and Figure 3 is a diagram with equal accuracy that can be measured using the pair of electronic scanning radar and mechanical scanning radar in Figure 1. FIG. 4 is a plan view of a contour line for nine cases in which two mechanical scanning radars are arranged in FIG. 1. 1...Electronic scanning two-dimensional radar, 2...
Mechanical scanning two-dimensional radar, 3...Receiver, 4.
...MTI. 5...Altitude calculation filter, 6...Monitoring instruction device, 7...Microwave communication device, 8.
...Transmission device. @Momo P tough f11 counterfeit Ecal γ

Claims (1)

【特許請求の範囲】[Claims] 目標の方位と距離を高精度で測定する電子走査アンテナ
を持つ第1の2次元レーダと、目標の距離を高精度で測
定する機械的走査アンテナを持つ複数の第2の2次元レ
ーダとを備えたレーダシステムのレーダ測高方式におい
て、追尾目標の位置によって前記第1のレーダと対とな
る前記第2のレーダの組合わせを変え、これら対となる
各レーダによってほぼ同時刻に前記目標の距離と方位を
それぞれ測定し、これら対となる両レーダの2組のデー
タから幾何学的に目標の高度を測定することを特徴とす
るレーダ測高方式。
A first two-dimensional radar having an electronic scanning antenna that measures the direction and distance of the target with high precision, and a plurality of second two-dimensional radars having mechanical scanning antennas that measure the distance of the target with high precision. In the radar height measurement method of a radar system, the combination of the first radar and the second radar paired with each other is changed depending on the position of the tracking target, and each of the paired radars measures the distance of the target at approximately the same time. This radar height measurement method is characterized in that the height of the target is measured geometrically from two sets of data from both paired radars.
JP25997785A 1985-11-19 1985-11-19 Radar altitude measuring system Pending JPS62119486A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP25997785A JPS62119486A (en) 1985-11-19 1985-11-19 Radar altitude measuring system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25997785A JPS62119486A (en) 1985-11-19 1985-11-19 Radar altitude measuring system

Publications (1)

Publication Number Publication Date
JPS62119486A true JPS62119486A (en) 1987-05-30

Family

ID=17341559

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25997785A Pending JPS62119486A (en) 1985-11-19 1985-11-19 Radar altitude measuring system

Country Status (1)

Country Link
JP (1) JPS62119486A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03273183A (en) * 1990-03-23 1991-12-04 Nec Corp Bistatic radar device
JP2009244194A (en) * 2008-03-31 2009-10-22 Nec Corp Radar device
JP2012088163A (en) * 2010-10-19 2012-05-10 Nec Corp Pulse radar apparatus, pulse radar apparatus control method and program for control thereof
CN110596660A (en) * 2019-10-09 2019-12-20 富临精工先进传感器科技(成都)有限责任公司 Method and system for improving accuracy of radar measurement object size

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03273183A (en) * 1990-03-23 1991-12-04 Nec Corp Bistatic radar device
JP2009244194A (en) * 2008-03-31 2009-10-22 Nec Corp Radar device
JP2012088163A (en) * 2010-10-19 2012-05-10 Nec Corp Pulse radar apparatus, pulse radar apparatus control method and program for control thereof
CN110596660A (en) * 2019-10-09 2019-12-20 富临精工先进传感器科技(成都)有限责任公司 Method and system for improving accuracy of radar measurement object size

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