JPH03125983A - Radar device - Google Patents

Radar device

Info

Publication number
JPH03125983A
JPH03125983A JP1265594A JP26559489A JPH03125983A JP H03125983 A JPH03125983 A JP H03125983A JP 1265594 A JP1265594 A JP 1265594A JP 26559489 A JP26559489 A JP 26559489A JP H03125983 A JPH03125983 A JP H03125983A
Authority
JP
Japan
Prior art keywords
vibration
actuator
antenna
radio
radio wave
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
JP1265594A
Other languages
Japanese (ja)
Inventor
Nobuo Kamei
亀井 信夫
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP1265594A priority Critical patent/JPH03125983A/en
Publication of JPH03125983A publication Critical patent/JPH03125983A/en
Pending legal-status Critical Current

Links

Landscapes

  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Support Of Aerials (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

PURPOSE:To protect the apparatus from effect of vibration by detecting a vibration velocity of an radio wave antenna to reduce vibration with application of a reverse braking force proportional to the vibration velocity. CONSTITUTION:A mobile mass 4 is mounted on a radar unit 1 free to move through a spring 5 and an actuator 6. An accelerometer 7 detects a vibration velocity of a radio wave antenna 2 with an integrator 9 of a controller 8 and an adverse braking force proportional to the vibration velocity is generated in the actuator 6 with a power amplifier 10. A fixed core 11 composes the actuator 6 together with a mobile core 12. With such an arrangement, a vibration controlling function is added to a radar unit 1 thereby achieving a higher directing accuracy of the antenna 2 and a reduction in effect of vibration on an onboard electronic equipment.

Description

【発明の詳細な説明】 (産業上の利用分野〕 この発明は1例えば車両等に搭載するレーダ装置の運用
時の振動低減に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to vibration reduction during operation of a radar device mounted on, for example, a vehicle.

〔従来の技術〕[Conventional technology]

近年開発される車両搭載用のレーダ装置は。 Vehicle-mounted radar equipment has been developed in recent years.

探知距離の増大、地表付近の障害物の影響除去、遮へい
物の陰からの運用などの目的で、地上よシ高い位置に電
波アンテナを位置させることができるような折シ畳み式
の架台等を備えたものが多い。これらのレーダ装置では
、運用時に不安定な架台上に電波アンテナがあるため、
車両振動や風等の影響で電波アンテナ部の摂動が増大し
、指向精度の低下や、搭載電子機器の信頼性の低下を招
いていた。
For purposes such as increasing detection distance, removing the influence of obstacles near the ground, and operating from behind shielding objects, we have installed a foldable mount that allows radio antennas to be positioned high above the ground. There are many things prepared. These radar devices have radio antennas on mounts that are unstable during operation.
Perturbations in the radio antenna section increased due to the effects of vehicle vibration, wind, etc., leading to a decrease in pointing accuracy and reliability of the onboard electronic equipment.

第6図は、従来のレーダ装置の概要を示したもので1口
)はレーダ装置、(2)は電波アンテナ。
Figure 6 shows an overview of a conventional radar device, where 1) is the radar device and (2) is a radio antenna.

(3)は架台である。上記LLごダ装置(11は、使用
時には架台(3)を展伸して1t1波アンテナ(2)を
見通しのよい高さKすることができるが、車両振動や風
の影響で、上記レーダ装&(1)全体に点線で示すよう
な振動が生じていた。このような振動は、電波アンテナ
の指向精度を損なうばかシでなく、搭載されている電子
機器の信頼性にも有害な影響を与える恐れがあった。
(3) is a pedestal. When in use, the LL radar device (11) can extend the mount (3) to raise the 1t1 wave antenna (2) to a height K with good visibility, but due to the effects of vehicle vibration and wind, the radar installation & (1) Vibrations as shown by the dotted line were occurring throughout the device.Such vibrations not only impair the pointing accuracy of the radio antenna, but also have a detrimental effect on the reliability of the electronic equipment installed. I was afraid of giving it away.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

レーダ装置に生じるこれらの振動を低減するために従来
、その対策として構造体の補強が施されていたが、レー
ダ装置の重量が増し、振動系が多少質れるだけで根本的
な対策とはなっていなかった。
In order to reduce these vibrations that occur in radar equipment, conventional measures have been to strengthen the structure, but this increases the weight of the radar equipment and only slightly improves the quality of the vibration system, but is not a fundamental countermeasure. It wasn't.

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、可動質量の反力を利用してレーダ装置に生じた振動
を低減する制御力を作用させ、撮動の影響を受は難いレ
ーダ装置を得ることを目的としている。
This invention was made to solve this problem, and uses the reaction force of a movable mass to apply a control force that reduces vibrations generated in a radar device, thereby making the radar device less susceptible to the effects of imaging. The purpose is to obtain.

〔課題を解決するための手段〕[Means to solve the problem]

この発明に係わるレーダ装置は、電波アンテナの振動速
度を検出し、この振動速度に比例した逆向きの制御力を
作用させることにより振動を低減させるようにしたもの
である。
The radar device according to the present invention detects the vibration speed of a radio wave antenna, and reduces vibration by applying a control force in the opposite direction that is proportional to the vibration speed.

〔作用〕[Effect]

この発明においては、アクチュエータが可動質素の反力
を利用して振動を有効に低減させる制御力をレーダ装&
に作用させるため車両振動や風による振動を大巾に減少
させることができ、を波アンテナ指向精度の向上や、搭
載されている電子装置に振動の影響を与えることを防止
することができる。
In this invention, the actuator uses the reaction force of the movable element to provide a control force that effectively reduces vibrations in the radar equipment and
Because it acts on vibrations, vehicle vibrations and wind-induced vibrations can be greatly reduced, improving the pointing accuracy of wave antennas and preventing the effects of vibrations on mounted electronic devices.

〔実施例〕〔Example〕

第1図はこの発明の一実施例を示す図であシ、(1)〜
(3)は上記従来装置と全く同一である。(4)は可動
質量で、バネ(5)とアクチュエータ(6)を介してレ
ーダ装置(1)K可動自在に取シ付けられている。(7
)は加速度計で、制御器(8)の積分器(9)によシミ
波アンテナ(2)の振動速度を検出し、電力増巾器α〔
によシアクチェエータ(6)に振動速度に比例した逆向
きの制御力を発生させている。Iは固定コアで、可動コ
アυとともにアクチュエータ(6)を構成する。
FIG. 1 is a diagram showing an embodiment of the present invention, (1) to
(3) is completely the same as the conventional device described above. (4) is a movable mass which is movably attached to the radar device (1)K via a spring (5) and an actuator (6). (7
) is an accelerometer that detects the vibration speed of the smear wave antenna (2) through the integrator (9) of the controller (8), and detects the vibration speed of the stain wave antenna (2).
A control force in the opposite direction proportional to the vibration speed is generated in the vibration actuator (6). I is a fixed core, which together with the movable core υ constitutes an actuator (6).

第2図は装置の動作を説明するモデル図で。Figure 2 is a model diagram explaining the operation of the device.

M、は電波アンテナ等の質素、に、はバネ定数00は減
衰定数であり1M、は可動質t(4)の質素+  ’l
はバネ(5)のバネ定数、(6)はアクチュエータであ
る。ここでX、を電波アンテナ(2)の撮動変位、x、
を可動質t (4)の変位にとると運動方程式は以下の
ようになる。
M, is the simplicity of a radio antenna, etc., is the spring constant, 00 is the damping constant, and 1M is the simplicity of the movable material t(4) + 'l
is the spring constant of spring (5), and (6) is the actuator. Here, X is the imaging displacement of the radio antenna (2), x,
If we take the displacement of the mobile body t (4), the equation of motion becomes as follows.

(Xl−X、)=F−V・・・・・・・・・・・・・・
・・・・(1)J  X、+に、(Xfi −Xj  
)=v、、、(21ここで制御力Vは、電波アンテナ(
2)の振動速度x1に比例しゲイン定数をCmとする次
のような形で発生させる。
(Xl-X,)=F-V・・・・・・・・・・・・・・・
...(1) J X, +, (Xfi -Xj
)=v,,,(21Here, the control force V is the radio antenna (
2) is generated in the following form, which is proportional to the vibration speed x1 and has a gain constant of Cm.

V=Omx1 (3) 式(3)を式(りに代入すると以下のようKなる。V=Omx1 (3) Substituting equation (3) into equation (ri) yields K as follows.

式(4)よシ制御をかけることによシ、振動系の見かけ
の減衰を、00から(Oo+Om)に増加させることに
よシ有効な撮動低減効果を得ていることがわかる。
It can be seen that by controlling the equation (4) and increasing the apparent damping of the vibration system from 00 to (Oo+Om), an effective photographic reduction effect can be obtained.

第3図はこの発明の他の実施例に係わるもので、第1図
における電波アンテナ(2)を複数装備し、可動質量(
4)を上記電波アンテナのほぼ重心位置に取シ付は九も
のである。この第3図によれば、車両振動や風等によシ
生じる振動速度Vに対し制御力Vを発生することにより
、複数の電波アンテナに生じる振動を効率良く低減でき
機構の単純化をはかることができる。
FIG. 3 relates to another embodiment of the present invention, which is equipped with a plurality of radio wave antennas (2) in FIG. 1, and has a movable mass (
4) is mounted approximately at the center of gravity of the radio antenna. According to FIG. 3, by generating a control force V against the vibration velocity V caused by vehicle vibrations, wind, etc., it is possible to efficiently reduce vibrations generated in multiple radio antennas and simplify the mechanism. Can be done.

第4図は、逆Km波アンテナ(2)に対し、可動質fl
(4)を複数個用いたもので、可動質−1i (41の
設置位置を自由に選ぶことができるようになる。
Figure 4 shows the movable material fl for the inverted Km wave antenna (2).
By using a plurality of (4), the installation position of the movable member-1i (41) can be freely selected.

第5図は、電波アンテナ(2)も可動質量(4)も複数
布するもので、複数の電波アンテナに対し設置位置の制
約を緩和して有利な位置が選べるようになる。
In FIG. 5, a plurality of radio wave antennas (2) and a plurality of movable masses (4) are arranged, so that restrictions on the installation positions of the plurality of radio wave antennas are relaxed and an advantageous position can be selected.

〔発明の効果〕〔Effect of the invention〕

(Xl   xt ) ==p・・・(4)この発明は
以上説明したとおυ、レーダ装置に振動制御機能を付与
することによシ、電波アンテナの指向精度の向上と、搭
載電子様器への撮動の影響を低減するという効果がある
(xl This has the effect of reducing the influence of photographing.

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

第1図はこの発明の一実施例を示す図、第2図は振動制
御の原理を示す図、第3〜5図は。 この発明の他の実施例を示す図、第6図は従来のレーダ
装置を示す図であ名。 図において(1)はレーダ装置、(2)は電波アンテナ
、(3)は架台、(4)は可動質量、(5)はバネ、(
6)はアクチュエータ、(7)は加速度計、(8)は制
御器である。
FIG. 1 is a diagram showing an embodiment of the present invention, FIG. 2 is a diagram showing the principle of vibration control, and FIGS. 3 to 5 are diagrams showing the principle of vibration control. FIG. 6 is a diagram showing another embodiment of the present invention, and FIG. 6 is a diagram showing a conventional radar device. In the figure, (1) is a radar device, (2) is a radio antenna, (3) is a pedestal, (4) is a movable mass, (5) is a spring, (
6) is an actuator, (7) is an accelerometer, and (8) is a controller.

Claims (3)

【特許請求の範囲】[Claims] (1)電波アンテナと、上記電波アンテナの振動を検出
する振動検査手段と、上記電波アンテナの振動方向に往
復動する可動質量と、上記可動質量を駆動するアクチュ
エータと、上記振動検査手段により検出された電波アン
テナの振動速度に比例した制御力を出力できるよう上記
アクチュエータを制御する制御器とを備えたことを特徴
とするレーダ装置。
(1) A radio antenna, a vibration inspection means for detecting the vibration of the radio antenna, a movable mass that reciprocates in the vibration direction of the radio antenna, an actuator that drives the movable mass, and a vibration inspection means that detects the vibration of the radio antenna. and a controller that controls the actuator so as to output a control force proportional to the vibration speed of the radio antenna.
(2)可動質量と電波アンテナのいづれか一方を複数個
とし、他方を上記一方のほぼ重心位置に取り付けたこと
を特徴とする特許請求の範囲第(1)項記載のレーダ装
置。
(2) A radar device according to claim (1), characterized in that either a plurality of movable masses or a plurality of radio wave antennas are provided, and the other is attached approximately to the center of gravity of the one.
(3)複数の電波アンテナと複数の可動質量を備え、上
記可動質量全体の重心を、上記電波アンテナ全体の重心
にほぼ一致させたことを特徴とする特許請求の範囲第(
1)項記載のレーダ装置。
(3) A plurality of radio wave antennas and a plurality of movable masses are provided, and the center of gravity of the entire movable mass is made to substantially coincide with the center of gravity of the entire radio wave antenna.
The radar device described in section 1).
JP1265594A 1989-10-12 1989-10-12 Radar device Pending JPH03125983A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1265594A JPH03125983A (en) 1989-10-12 1989-10-12 Radar device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1265594A JPH03125983A (en) 1989-10-12 1989-10-12 Radar device

Publications (1)

Publication Number Publication Date
JPH03125983A true JPH03125983A (en) 1991-05-29

Family

ID=17419293

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1265594A Pending JPH03125983A (en) 1989-10-12 1989-10-12 Radar device

Country Status (1)

Country Link
JP (1) JPH03125983A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111555016B (en) * 2020-05-12 2021-04-20 北京无线电测量研究所 Airborne radar antenna damping device

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59161101A (en) * 1983-02-14 1984-09-11 トラコ−,ベイ,インコ−ポレ−テツド Stable antenna unit with accelerating moving mass
JPS607202A (en) * 1983-06-27 1985-01-16 Toshiba Corp Stabilizer
JPS6271307A (en) * 1985-09-25 1987-04-02 Nippon Telegr & Teleph Corp <Ntt> Antenna stabilizer
JPS62112403A (en) * 1985-11-12 1987-05-23 Nippon Kokan Kk <Nkk> Ship radar with stabilizer

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59161101A (en) * 1983-02-14 1984-09-11 トラコ−,ベイ,インコ−ポレ−テツド Stable antenna unit with accelerating moving mass
JPS607202A (en) * 1983-06-27 1985-01-16 Toshiba Corp Stabilizer
JPS6271307A (en) * 1985-09-25 1987-04-02 Nippon Telegr & Teleph Corp <Ntt> Antenna stabilizer
JPS62112403A (en) * 1985-11-12 1987-05-23 Nippon Kokan Kk <Nkk> Ship radar with stabilizer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111555016B (en) * 2020-05-12 2021-04-20 北京无线电测量研究所 Airborne radar antenna damping device

Similar Documents

Publication Publication Date Title
US20200361629A1 (en) Stabilizing platform
JP6051327B1 (en) Unmanned aerial vehicle
US7240754B2 (en) Truck cab suspension control
CA2568423A1 (en) System for anticipated measurement of turbulence upstream of an aircraft
CN105501454B (en) A kind of miniature gondola
US4315610A (en) Optical image stabilizing system
CN109945861B (en) Alignment tracking device and method for unidirectional wireless optical communication between small unmanned aerial vehicle and ground
CN104903790A (en) Apparatus and methods for stabilization and vibration reduction
CN103277640B (en) Vehicle-mounted two-shaft photographing tripod head
WO2019091419A1 (en) Control method for augmenting drone stabilization, device and drone
CN110645311B (en) Formula of sweeping photoelectricity stabilising arrangement that takes photo by plane
CN206552283U (en) A kind of equipment of taking photo by plane applied to unmanned plane
JPH03125983A (en) Radar device
US8379190B2 (en) Resonant scanner for 3D mapping
CN109029436B (en) Triaxial inertially stabilized platform
JPH08239100A (en) Support structure of loaded equipment for unmanned helicopter
US6122102A (en) Sighting apparatus for aiming an optical device
CN208915460U (en) A kind of fire-fighting unmanned plane lighting device convenient for handling
JPH04306197A (en) On-board pod for aircraft
CN213620282U (en) Cantilever type fixing device for image collector
CN212572724U (en) Anti-overload image acquisition device
JPS6141032A (en) Vibration controller
JPS6057030A (en) Vibration control equipment
CN211592148U (en) Intelligent patrol robot
CN204906537U (en) A road monitoring camera anti -shake device for compensating cantilever beam sways