JPS6269177A - Rader equipment - Google Patents
Rader equipmentInfo
- Publication number
- JPS6269177A JPS6269177A JP60210669A JP21066985A JPS6269177A JP S6269177 A JPS6269177 A JP S6269177A JP 60210669 A JP60210669 A JP 60210669A JP 21066985 A JP21066985 A JP 21066985A JP S6269177 A JPS6269177 A JP S6269177A
- Authority
- JP
- Japan
- Prior art keywords
- distance resolution
- voltage
- signal
- vco
- section
- 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
Links
Landscapes
- Radar Systems Or Details Thereof (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
本発明は人工衛星又航空機等の飛翔体に塔載されたレー
ダ装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a radar device mounted on a flying object such as an artificial satellite or an aircraft.
[従来の技術]
従来の人工衛星又は航空機等に塔載されたレーダ装置で
あるサイドルッキングレーダにおいては、送信パルスの
ピーク値出力を増大させずに所要の平均電力を確保する
ため、いわゆるブルス圧縮技術が用いられている。これ
は送信パルスを狭くする代わりにパルス幅を長くしてこ
れに線形周波数変調(リニアFM)を加えて、信号の占
有帯域幅を広くし、受信後周波数対遅延時間特性が逆な
分散型遅延線を通すか又はそれと等価なマツチドフィル
タ(Matched Filter)を通し信号内エネ
ルギーが一点に集積され尖鋭なパルスを出力させる技術
である。この場合距離分離能δrは、第2図のジオメト
リ図に示すように、信号帯域幅をΔf、光速をC1仰角
をψとすれば(1)式で表わされる。[Prior Art] In side-looking radar, which is a radar device mounted on a conventional artificial satellite or aircraft, so-called bulls compression is used to ensure the required average power without increasing the peak value output of the transmitted pulse. technology is used. Instead of narrowing the transmitted pulse, it lengthens the pulse width and adds linear frequency modulation (linear FM) to it, widening the occupied bandwidth of the signal, and after receiving it, it uses a distributed delay system with reverse frequency vs. delay time characteristics. This is a technique in which the energy in the signal is concentrated at one point through a wire or an equivalent matched filter, and a sharp pulse is output. In this case, the distance separation power δr is expressed by equation (1), as shown in the geometry diagram of FIG. 2, where the signal bandwidth is Δf, the speed of light is C1, and the elevation angle is ψ.
δ・= 0・nu・ 1・−1−(1)■ π 7
Vf−cosψ
また、仰角ψは高度H1地球半径Re、オフナディア角
αを用い次の式から求められる。δ・=0・nu・1・−1−(1) ■ π 7
Vf-cos ψ Also, the elevation angle ψ is obtained from the following equation using the altitude H1, the earth's radius Re, and the off-nadir angle α.
Re+H。Re+H.
ψ = cas ” ((−f丁−) sin a’
t (2)[解決すべき問題点]
上述した従来のパルス圧縮技術を用いたレーダ装置では
、信号帯域幅Δfが固定のため距離分解能を可変するた
めにはオフナディア角αを変えるしかなく、同−オフナ
ディア角で異なる分解能を得ることができない欠点があ
った。ψ = cas ” ((-f d-) sin a'
t (2) [Problems to be solved] In the radar device using the conventional pulse compression technology described above, the signal bandwidth Δf is fixed, so the only way to vary the distance resolution is to change the off-nadir angle α. There is a drawback that different resolutions cannot be obtained at the same off-nadir angle.
[問題点の解決手段]
上記問題点を解決する本発明のレーダ装置は、航空機な
どの飛翔体に塔載されたレーダ装置において、電圧を制
御することにより発振周波数を変えることができる電圧
制御発振部と外部からのコマンド又は制御信号により任
意の距離分解能を達成するのに最適な信号の帯域幅を求
め前記電圧制御発振部の電圧制御範囲を決める制御部と
を備え、前記電圧制御発振部の発振周波数を制御するこ
とにより信号帯域幅を変え、あるオフナディア角に対し
距離分解能を可変することができる構成である。[Means for Solving the Problems] The radar device of the present invention that solves the above problems is a radar device mounted on a flying object such as an aircraft, which uses voltage-controlled oscillation in which the oscillation frequency can be changed by controlling the voltage. and a control unit that determines the optimal signal bandwidth to achieve a desired distance resolution using an external command or control signal and determines the voltage control range of the voltage controlled oscillation unit, By controlling the oscillation frequency, the signal bandwidth can be changed and the distance resolution can be varied for a certain off-nadir angle.
[実施例]
以下、本発明につき好適なる一実施例を示す同面を用い
て詳細に説明する。[Example] Hereinafter, the present invention will be described in detail using the same drawing showing a preferred example.
第1図は本発明の一実施例に係るレーダ装置のブロック
図である。FIG. 1 is a block diagram of a radar device according to an embodiment of the present invention.
本実施例のレーダ装置は、基準信号発生部1、Vco電
圧制御発振部2、発振部3.受信部4゜アイソレータ5
、アンテナ6及びVco制御演算部7から構成される。The radar device of this embodiment includes a reference signal generation section 1, a Vco voltage controlled oscillation section 2, an oscillation section 3. Receiving section 4゜Isolator 5
, an antenna 6, and a Vco control calculation section 7.
基準信号発生部1は基準となる任意の周波数信号を発生
する機能を有し、送信部3はVco電圧制御発振部2で
制御された送信信号を所定のレベルまで増幅し、アイソ
レータ5を介してアンテナ部6に出力する機能を有し、
受信部4はアンテナ部出力の受信信号を増幅しローカル
信号で検波してビデオ信号を作り出す機能を有し、アン
テナ部6はレーダ信号の送受信機能を有する。The reference signal generator 1 has a function of generating an arbitrary frequency signal as a reference, and the transmitter 3 amplifies the transmit signal controlled by the Vco voltage control oscillator 2 to a predetermined level, and transmits the signal via the isolator 5. It has a function of outputting to the antenna section 6,
The receiving section 4 has a function of amplifying the received signal output from the antenna section and detecting it with a local signal to create a video signal, and the antenna section 6 has a function of transmitting and receiving radar signals.
Vco電圧制御発振部2は基準信号発生部1の出力信号
と同期し、Vco制御演算部7からの電圧制御信号によ
り発振周波数を制御し、所望の距離分解能に対応した信
号帯域幅になるよう周波数掃引幅を制御する機能を有す
る。又、Vco制御演算部7は所望の距離分解能情報を
含むコマンド又は制御信号をデコードし基準信号発生部
1の出力である周波数を中心にVco電圧制御発振部2
の距離分解能に対応した周波数掃引幅を制御する電圧制
御信号を発生する機能を有する。The Vco voltage control oscillation unit 2 is synchronized with the output signal of the reference signal generation unit 1, controls the oscillation frequency by the voltage control signal from the Vco control calculation unit 7, and adjusts the frequency so that the signal bandwidth corresponds to the desired distance resolution. It has a function to control the sweep width. Further, the Vco control calculation section 7 decodes the command or control signal including desired distance resolution information, and generates the Vco voltage control oscillation section 2 around the frequency that is the output of the reference signal generation section 1.
It has the function of generating a voltage control signal that controls the frequency sweep width corresponding to the distance resolution of .
以上の如く本実施例のレーダ装置は、所望の距離分解能
に対応するコマンド又は制御信号によりVco制御演算
部7でVco電圧制御発振部2を制御し、Vco電圧制
御発振部2で制御する発振周波数の信号帯域幅を所望の
距離分解能に対応した信号帯域幅に変えるようにしたの
で、に記した(1)及び(2)式から明らかなように信
号帯域幅Δfが固定である従来と異なりオフナディア角
αを変化させることなく距離分解能を可変とすることが
可能となる。As described above, in the radar device of this embodiment, the Vco control calculation unit 7 controls the Vco voltage control oscillation unit 2 using a command or control signal corresponding to a desired distance resolution, and the oscillation frequency controlled by the Vco voltage control oscillation unit 2 Since the signal bandwidth of Δf is changed to the signal bandwidth corresponding to the desired distance resolution, unlike the conventional case where the signal bandwidth Δf is fixed, as is clear from equations (1) and (2) described in It becomes possible to make the distance resolution variable without changing the nadir angle α.
[発明の効果コ
以上説明したように本発明は、所望の距離分解能に対応
したコマンド又は制御信号によりVc。[Effects of the Invention] As explained above, the present invention provides Vc by a command or control signal corresponding to a desired distance resolution.
電圧制御発振部の電圧制御を行い、送信信号の信号帯域
幅を距離分解能に対応した所定の帯域幅に制御すること
を可能とすることにより、オフナディア角を変化させる
ことなくレーダの距離分解能を可変にでき同じオフナデ
ィア角、つまり同一目標に対し種々の分解能が得られる
効果がある。By controlling the voltage of the voltage controlled oscillator and controlling the signal bandwidth of the transmitted signal to a predetermined bandwidth corresponding to the distance resolution, the distance resolution of the radar can be improved without changing the off-nadir angle. This has the effect of being variable and providing various resolutions for the same off-nadir angle, that is, the same target.
第1図は本発明の一実施例に係るレーダ装置のブロック
図、
第2図は航空機等に塔載されるサイドルッキングレーダ
のジオメトリ図である。
1:基準信号発振部
2:Vco電圧制御発振部
3:送信部
4:受信部
5ニアイソレータ
6:アンテナ部
7:Vco制御演算部FIG. 1 is a block diagram of a radar device according to an embodiment of the present invention, and FIG. 2 is a geometry diagram of a side-looking radar mounted on an aircraft or the like. 1: Reference signal oscillation section 2: Vco voltage control oscillation section 3: Transmission section 4: Receiving section 5 Near isolator 6: Antenna section 7: Vco control calculation section
Claims (1)
電圧を制御することにより発振周波数を変えることがで
きる電圧制御発振部と外部からのコマンド又は制御信号
により任意の距離分解能を達成するのに最適な信号の帯
域幅を求め前記電圧制御発振部の電圧制御範囲を決める
制御部とを備え、前記電圧制御発振部の発振周波数を制
御することにより信号帯域幅を変え、あるオフナディア
角に対し距離分解能を可変することができることを特徴
とするレーダ装置。In radar equipment mounted on flying objects such as aircraft,
A voltage controlled oscillator whose oscillation frequency can be changed by controlling the voltage and an external command or control signal are used to determine the optimal signal bandwidth to achieve a desired distance resolution and calculate the voltage of the voltage controlled oscillator. A radar device comprising: a control section that determines a control range; the signal bandwidth can be changed by controlling the oscillation frequency of the voltage-controlled oscillation section, and the distance resolution can be varied for a certain off-nadir angle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP60210669A JPS6269177A (en) | 1985-09-24 | 1985-09-24 | Rader equipment |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP60210669A JPS6269177A (en) | 1985-09-24 | 1985-09-24 | Rader equipment |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6269177A true JPS6269177A (en) | 1987-03-30 |
Family
ID=16593148
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP60210669A Pending JPS6269177A (en) | 1985-09-24 | 1985-09-24 | Rader equipment |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6269177A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06102342A (en) * | 1992-06-08 | 1994-04-15 | Hughes Aircraft Co | Low noise microwave wide band signal generator |
KR101702581B1 (en) * | 2015-12-15 | 2017-02-03 | 국방과학연구소 | An apparatus for processing a radar scan image and method therfor |
-
1985
- 1985-09-24 JP JP60210669A patent/JPS6269177A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH06102342A (en) * | 1992-06-08 | 1994-04-15 | Hughes Aircraft Co | Low noise microwave wide band signal generator |
KR101702581B1 (en) * | 2015-12-15 | 2017-02-03 | 국방과학연구소 | An apparatus for processing a radar scan image and method therfor |
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