JPH0792470B2 - Impact detection identification mechanism - Google Patents
Impact detection identification mechanismInfo
- Publication number
- JPH0792470B2 JPH0792470B2 JP3297814A JP29781491A JPH0792470B2 JP H0792470 B2 JPH0792470 B2 JP H0792470B2 JP 3297814 A JP3297814 A JP 3297814A JP 29781491 A JP29781491 A JP 29781491A JP H0792470 B2 JPH0792470 B2 JP H0792470B2
- Authority
- JP
- Japan
- Prior art keywords
- collision
- acceleration sensor
- hollow structure
- output
- acceleration
- 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.)
- Expired - Lifetime
Links
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Description
【0001】[0001]
【産業上の利用分野】本発明は、物体の衝突時に衝突条
件を検知識別する衝撃検知識別機構に関するものであ
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an impact detection / identification mechanism for detecting and identifying a collision condition when an object collides.
【0002】[0002]
【従来の技術】従来、物体の衝突を検知する機構として
は、慣性スイッチ、破壊スイッチ、振動センサ、加速度
センサ等が用いられており、衝突時の減加速度、物体変
形、振動を検知している。また、衝突条件の識別は、一
定値以上の減加速度、変形、振動を検出すること等によ
り衝突とそれ以外の衝撃の弁別を行っている。しかし、
これらの方式では、衝突速度、衝突角度、衝突した物体
の材質等の衝突条件の識別は不可能であった。2. Description of the Related Art Conventionally, an inertia switch, a breaking switch, a vibration sensor, an acceleration sensor, etc. have been used as a mechanism for detecting a collision of an object, and detect deceleration, object deformation and vibration at the time of collision. . Further, the collision condition is identified by detecting a deceleration, a deformation, a vibration or the like having a certain value or more to discriminate between the collision and other impacts. But,
With these methods, it is impossible to identify the collision conditions such as the collision speed, the collision angle, and the material of the collision object.
【0003】[0003]
【発明が解決しようとする課題】本発明は、上記の実情
に鑑みてなされるもので、衝突速度、衝突角度、衝突し
た物体の材質等を衝突時に検知識別可能な衝撃検知識別
機構を提供することをその目的とするものである。SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and provides an impact detection / identification mechanism capable of detecting and identifying the collision speed, the collision angle, the material of a collided object, and the like at the time of collision. That is the purpose.
【0004】[0004]
【課題を解決するための手段】本発明に係る衝撃検知識
別機構は、上記課題を解決するため、 a 中空構造体内に取り付けられていて、該中空構造体
と物体の衝突によって生じた当該中空構造体を伝わる衝
撃波を検知する加速度センサと、 b 前記中空構造体内に収納されていて、前記加速度セ
ンサの出力である衝撃波形を周波数帯域別に弁別するフ
ィルタ回路と、 c 前記中空構造体内に収納されていて、前記フィルタ
回路の出力波形と衝突条件との相関関係から、周波数帯
域別の加速度値を変数とした計算式を計算して衝突条件
を算出する演算回路とを備えた構成としている。In order to solve the above-mentioned problems, an impact detection / identification mechanism according to the present invention is mounted in a hollow structure a and is generated by a collision between the hollow structure and an object. An acceleration sensor for detecting a shock wave propagating through the hollow structure; and a filter circuit housed in the hollow structure for discriminating a shock waveform output from the acceleration sensor into frequency bands. , C is housed in the hollow structure , and the frequency band is determined from the correlation between the output waveform of the filter circuit and the collision condition.
An arithmetic circuit for calculating a collision condition by calculating a calculation formula using the acceleration value for each region as a variable is configured.
【0005】[0005]
【作用】本発明の衝撃検知識別機構においては、加速度
センサ出力の高周波域と低周波域では、衝突速度、衝突
角度、衝突体の材質等に対する応答が異なることに着目
し、加速度センサ出力をフィルタ回路で周波数帯域別に
弁別したものを演算回路に入力して衝突条件を識別する
ようにしている。In the impact detection / identification mechanism of the present invention, the acceleration sensor output is filtered by focusing on the fact that the response to the collision speed, the collision angle, the material of the collision body, etc. is different in the high frequency region and the low frequency region of the acceleration sensor output. The circuit discriminates by frequency band is input to the arithmetic circuit to identify the collision condition.
【0006】[0006]
【実施例】以下、本発明に係る衝撃検知識別機構の実施
例を図面に従って説明する。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of a shock detection / identification mechanism according to the present invention will be described below with reference to the drawings.
【0007】図1は本発明の実施例を示すブロック図で
あり、中空で強固な構造体1内には、加速度センサ4、
フィルタ回路5及び演算回路6が収納されている。ここ
で、加速度センサ4は例えば構造体1の先端部の厚肉部
分に取り付けられて衝突時に発生して構造体1を伝わる
衝撃波を直接受け得るようになっている。フィルタ回路
5は加速度センサ4の出力の衝撃波形を周波数帯域別に
弁別するものであり、演算回路6はフィルタ回路5の各
周波数帯域別に弁別された出力波形から衝突条件を算出
し、衝突条件算出結果7を出力するものである。FIG. 1 is a block diagram showing an embodiment of the present invention. In a hollow and strong structure 1, an acceleration sensor 4,
The filter circuit 5 and the arithmetic circuit 6 are housed. Here, the acceleration sensor 4 is attached to, for example, a thick portion of the tip of the structure 1 so as to directly receive a shock wave generated in a collision and transmitted through the structure 1. The filter circuit 5 discriminates the impact waveform of the output of the acceleration sensor 4 for each frequency band, and the arithmetic circuit 6 calculates the collision condition from the output waveform discriminated for each frequency band of the filter circuit 5, and the collision condition calculation result. 7 is output.
【0008】図1の構成において、前記構造体1と衝突
体2が衝突すると、衝撃波3が発生し、これを構造体内
部の加速度センサ4で検出する。図2は加速度センサ4
の出力である検出波形の一例を示すものである。この加
速度センサ4で検出される衝撃波形は、衝突速度、衝突
角度、衝突した物体の材質等の衝突条件による影響の受
け方が周波数帯域によって異なる。In the structure shown in FIG. 1, when the structure 1 collides with the collision body 2, a shock wave 3 is generated, which is detected by the acceleration sensor 4 inside the structure. 2 shows the acceleration sensor 4
3 shows an example of a detected waveform that is the output of the. The impact waveform detected by the acceleration sensor 4 is affected by a collision condition such as a collision velocity, a collision angle, a material of a collided object, etc., depending on a frequency band.
【0009】その一例として、図3に示すように構造体
1が鋼板8に衝突しそれを貫徹した場合を考えると、構
造体内部の加速度センサ4で検出される加速度値(ピー
ク値)の衝突速度及び鋼板板厚に対するグラフは図4及
び図5のようになる。これを、加速度センサ出力の高周
波と低周波について分離してみると(例えば10kHzよ
り上を高周波域、10kHzより下を低周波域とする
と)、図6に示すように衝突速度と加速度値の関係で
は、センサ出力aの高周波域b及び低周波域cはそれぞ
れ衝突速度の増加に伴って増大しているが、高周波域b
は増大の程度が大きく低周波域cは増大の程度が小さ
い。また、図7の鋼板板厚と加速度値の関係でも、セン
サ出力dの高周波域e及び低周波域fはそれぞれ鋼板板
厚の増加に伴って増大しているが、高周波域eは増大の
程度が小さく低周波域fは増大の程度が大きい。このよ
うに加速度センサ出力は、周波数帯域によって衝突条件
の影響の受け方が違う。As an example, when the structure 1 collides with the steel plate 8 and penetrates it as shown in FIG. 3, the collision of the acceleration value (peak value) detected by the acceleration sensor 4 inside the structure. The graphs for speed and steel plate thickness are shown in FIGS. 4 and 5. When this is separated for the high frequency and the low frequency of the acceleration sensor output (for example, the high frequency region above 10 kHz is the low frequency region below 10 kHz), the relationship between the collision speed and the acceleration value is shown in FIG. In the high frequency range b and the low frequency range c of the sensor output a, the high frequency range b and the low frequency range c respectively increase as the collision speed increases.
Indicates a large increase and the low frequency range c indicates a small increase. Also, in the relationship between the steel plate thickness and the acceleration value in FIG. 7, the high-frequency range e and the low-frequency range f of the sensor output d increase with the increase of the steel plate thickness, but the high-frequency range e increases. Is small, and the low-frequency range f has a large degree of increase. In this way, the acceleration sensor output is affected by the collision condition depending on the frequency band.
【0010】周波数帯域別に各種衝突条件からの影響の
受け方が違うことから、各種衝突条件を未知数とした方
程式を、周波数帯域別の加速度値を変数として作ること
が可能となる。この方程式に、周波数帯域別の加速度値
を代入することにより、各種衝突条件を求めることがで
きる。図6の場合衝突速度の算出が、図7の場合鋼板板
厚の算出が可能となる。Since the influence of various collision conditions is different for each frequency band, it is possible to make an equation in which various collision conditions are unknowns by using the acceleration value for each frequency band as a variable. By substituting the acceleration value for each frequency band into this equation, various collision conditions can be obtained. In the case of FIG. 6, the collision speed can be calculated, and in the case of FIG. 7, the steel plate thickness can be calculated.
【0011】本発明では、このような加速度センサ出力
の特性を利用している。そして、加速度センサ出力をフ
ィルタ回路5に入力する。フィルタ回路5では加速度セ
ンサ出力を周波数帯域別に弁別する。この周波数帯域別
のフィルタ回路出力は上述したようにそれぞれ衝突条件
の異なった影響を受けている。当該フィルタ回路出力を
演算回路6で演算して、衝突条件算出結果7を得る。演
算回路6は、各種衝突条件を未知数とし、周波数帯域別
の加速度値を変数とした方程式を用いて演算し、各種衝
突条件を求める。The present invention utilizes such characteristics of the acceleration sensor output. Then, the output of the acceleration sensor is input to the filter circuit 5. The filter circuit 5 discriminates the acceleration sensor output for each frequency band. The output of the filter circuit for each frequency band is affected by different collision conditions as described above. The output of the filter circuit is calculated by the calculation circuit 6 to obtain the collision condition calculation result 7. The arithmetic circuit 6 calculates various collision conditions by using equations in which various collision conditions are unknowns and acceleration values for each frequency band are variables.
【0012】以下の式(1)は衝突条件の一つである衝
突速度Vを未知数とし、高周波域の加速度値をG1、低
周波域の加速度値をG2とした場合の方程式の1例であ
る。 V=αG1+βG2+γ …(1) (但し、α,β,γは加速度センサによって定まる定
数) α,β,γは実験により既知とすることができるから、
加速度値G1,G2を式(1)に代入することで衝突速度
Vを求めることができる。The following equation (1) is an example of an equation in which the collision velocity V, which is one of the collision conditions, is an unknown number, the acceleration value in the high frequency range is G 1 , and the acceleration value in the low frequency range is G 2. Is. V = αG 1 + βG 2 + γ (1) (where α, β, γ are constants determined by the acceleration sensor) Since α, β, γ can be known by experiments,
The collision speed V can be obtained by substituting the acceleration values G 1 and G 2 into the equation (1).
【0013】なお、演算式は演算回路6にプログラムし
ておく。また、フィルタ回路5及び演算回路6は、アナ
ログ回路又はデジタル回路を使用する。The arithmetic expression is programmed in the arithmetic circuit 6. Further, the filter circuit 5 and the arithmetic circuit 6 use an analog circuit or a digital circuit.
【0014】さらに、演算回路6としてデジタル回路を
使用する場合、(1)式のような方程式の演算を行う代
わりに、フィルタ回路5の高周波域及び低周波域の加速
度値出力についてそれぞれ特定のしきい値(1段階又は
複数段階のしきい値)を設定し、該しきい値を越えるか
否かで未知の衝突条件を求める演算処理を実行しても良
い。なお、衝突角度等の識別も同様に周波数帯域別のフ
ィルタ回路出力を演算処理して得られる。Further, when a digital circuit is used as the arithmetic circuit 6, instead of performing the arithmetic operation of the equation (1), the acceleration value output in the high frequency region and the low frequency region of the filter circuit 5 are respectively specified. It is also possible to set a threshold value (threshold value of one step or a plurality of steps) and execute an arithmetic process for obtaining an unknown collision condition depending on whether or not the threshold value is exceeded. The identification of the collision angle and the like can be similarly obtained by performing arithmetic processing on the filter circuit output for each frequency band.
【0015】[0015]
【発明の効果】本発明は以上の構成に基づくものであっ
て、中空構造体と物体の衝突によって発生する衝撃波を
中空構造体内の加速度センサにて検知し、その衝撃波を
フィルタ回路を通した得た周波数帯域別の加速度値を演
算回路で演算処理して各種衝突条件を算出するものであ
るから、物体の衝突を検知識別する機構(例えば砲弾等
の信管)に適用して極めて有効である。EFFECTS OF THE INVENTION The present invention is based on the above-mentioned constitution, and is capable of absorbing a shock wave generated by collision between a hollow structure and an object.
The shock wave is detected by the acceleration sensor inside the hollow structure.
The acceleration value for each frequency band obtained through the filter circuit is calculated.
Since a calculation circuit is used to calculate various collision conditions, a mechanism for detecting and identifying a collision of an object (for example, a shell or the like)
Is very effective when applied to.
【図1】本発明に係る衝撃検知識別機構の実施例を示す
構成図である。FIG. 1 is a configuration diagram showing an embodiment of an impact detection / identification mechanism according to the present invention.
【図2】加速度センサ検出波形の一例を示す波形図であ
る。FIG. 2 is a waveform diagram showing an example of an acceleration sensor detection waveform.
【図3】鋼板に衝突し貫徹した構造体の状態の説明図で
ある。FIG. 3 is an explanatory diagram of a state of a structure that has collided with a steel plate and penetrated.
【図4】図3で示す衝突において、衝突速度に対応した
加速度センサ出力の加速度値を示すグラフである。4 is a graph showing an acceleration value of an acceleration sensor output corresponding to a collision speed in the collision shown in FIG.
【図5】図3で示す衝突において、鋼板板厚に対応した
加速度センサ出力の加速度値を示すグラフである。5 is a graph showing the acceleration value of the acceleration sensor output corresponding to the steel plate thickness in the collision shown in FIG.
【図6】図4の加速度値を周波数帯域別に示したグラフ
である。6 is a graph showing the acceleration values of FIG. 4 for each frequency band.
【図7】図5の加速度値を周波数帯域別に示したグラフ
である。FIG. 7 is a graph showing the acceleration values of FIG. 5 for each frequency band.
1 構造体 2 衝突体 3 衝撃波 4 加速度センサ 5 フィルタ回路 6 演算回路 7 衝突条件算出結果 8 鋼板 1 Structure 2 Collision Body 3 Shock Wave 4 Acceleration Sensor 5 Filter Circuit 6 Calculation Circuit 7 Collision Condition Calculation Result 8 Steel Plate
───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平3−223676(JP,A) 特開 平3−67175(JP,A) 特開 平2−205727(JP,A) 特開 昭62−194421(JP,A) 特開 平4−224440(JP,A) 特開 平3−208751(JP,A) 特開 平3−223676(JP,A) 特開 平3−67175(JP,A) 特開 平2−205727(JP,A) 特開 昭62−194421(JP,A) 特開 平4−224440(JP,A) 特開 平3−208751(JP,A) ─────────────────────────────────────────────────── --- Continuation of the front page (56) Reference JP-A-3-223676 (JP, A) JP-A-3-67175 (JP, A) JP-A-2-205727 (JP, A) JP-A-62-1 194421 (JP, A) JP 4-224440 (JP, A) JP 3-208751 (JP, A) JP 3-223676 (JP, A) JP 3-67175 (JP, A) JP-A-2-205727 (JP, A) JP-A-62-194421 (JP, A) JP-A-4-224440 (JP, A) JP-A-3-208751 (JP, A)
Claims (1)
中空構造体と物体の衝突によって生じた当該中空構造体
を伝わる衝撃波を検知する加速度センサと、前記中空構造体内に収納されていて、前記 加速度センサ
の出力である衝撃波形を周波数帯域別に弁別するフィル
タ回路と、前記中空構造体内に収納されていて、前記 フィルタ回路
の出力波形と衝突条件との相関関係から、周波数帯域別
の加速度値を変数とした計算式を計算して衝突条件を算
出する演算回路とを備えたことを特徴とする衝撃検知識
別機構。1. Attached in a hollow structure,
Hollow structure produced by collision between hollow structure and object
An acceleration sensor for detecting a shock wave traveling through the, have been accommodated in the hollow structure, wherein a filter circuit for discriminating a shock wave for each frequency band which is an output of the acceleration sensor, have been accommodated in the hollow structure, wherein From the correlation between the output waveform of the filter circuit and the collision condition,
And a calculation circuit for calculating a collision condition by calculating a calculation formula using the acceleration value of 1. as a variable .
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3297814A JPH0792470B2 (en) | 1991-10-19 | 1991-10-19 | Impact detection identification mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3297814A JPH0792470B2 (en) | 1991-10-19 | 1991-10-19 | Impact detection identification mechanism |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH05107258A JPH05107258A (en) | 1993-04-27 |
JPH0792470B2 true JPH0792470B2 (en) | 1995-10-09 |
Family
ID=17851509
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3297814A Expired - Lifetime JPH0792470B2 (en) | 1991-10-19 | 1991-10-19 | Impact detection identification mechanism |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0792470B2 (en) |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5034891A (en) * | 1989-11-03 | 1991-07-23 | Trw Vehicle Safety Systems Inc. | Method and apparatus for sensing a vehicle crash with frequency domain boost |
US5036467A (en) * | 1990-04-04 | 1991-07-30 | Trw Vehicle Safety Systems Inc. | Method and apparatus for sensing a vehicle crash in real time using a frequency domain integration and summation algorithm |
-
1991
- 1991-10-19 JP JP3297814A patent/JPH0792470B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH05107258A (en) | 1993-04-27 |
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