JPH09159397A - Method and apparatus for controlling attitude of towing body - Google Patents

Method and apparatus for controlling attitude of towing body

Info

Publication number
JPH09159397A
JPH09159397A JP7320603A JP32060395A JPH09159397A JP H09159397 A JPH09159397 A JP H09159397A JP 7320603 A JP7320603 A JP 7320603A JP 32060395 A JP32060395 A JP 32060395A JP H09159397 A JPH09159397 A JP H09159397A
Authority
JP
Japan
Prior art keywords
attitude
towed
towing
mother
towed body
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.)
Granted
Application number
JP7320603A
Other languages
Japanese (ja)
Other versions
JP2682525B2 (en
Inventor
Yoshiyuki Murai
善幸 村井
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 JP7320603A priority Critical patent/JP2682525B2/en
Publication of JPH09159397A publication Critical patent/JPH09159397A/en
Application granted granted Critical
Publication of JP2682525B2 publication Critical patent/JP2682525B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To attempt to increase the moving range of a towing body by making it possible to control the attitude of the body by following up the attitude change of a mother aircraft or ship, thereby attempting to prevent the breakage accident of a towing cable, and alleviating the limit of the mobility of the mother aircraft or ship. SOLUTION: The apparatus for controlling the attitude of a towing body 1 to be towed by a mother aircraft or ship via a towing cable 2 comprises a tension sensor 11 for sensing the components of the tension applied to the cable 2 in longitudinal and lateral directions, a control calculator 12 for calculating the pitch and roll control amounts of the body 1 based on the components of the tension sensed by the sensor 11 in the longitudinal and lateral directions, and a driver 13 for driving the movable wings 1a of the body 1 based on the calculated result of the calculator 12.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、母機又は母船に曳
航索を介して曳航される曳航体の姿勢制御方法及び制御
装置に関し、特に、曳航索の破断事故の防止を図ること
ができる曳航体の姿勢制御方法及び姿勢制御装置に関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a attitude control method and control device for a towed body towed by a mother machine or a mother ship via a towline, and more particularly to a towed body capable of preventing breakage of the towline. Attitude control method and attitude control device.

【0002】[0002]

【従来の技術】従来から対空火器の標的や水中危険物の
処理等には、図5に示すように、母機(航空機)又は母
船(船舶)に曳航索102を介して曳航される曳航体1
01が広く用いられている。そして、このような曳航体
101を備えた従来の装置では、母機から曳航体101
を切り離した後に、繰り出される曳航索102に加わる
衝撃を軽減することにより、曳航索102の破断事故の
防止を図ったものが多数存在していた。
2. Description of the Related Art Conventionally, as shown in FIG. 5, a towed body 1 towed by a mother machine (aircraft) or a mother ship (ship) via a tow line 102 has been used for treating targets of an anti-aircraft firearm or underwater dangerous materials.
01 is widely used. Then, in the conventional device including such towed body 101, the towed body 101
There have been many attempts to prevent breakage accidents of the towline 102 by reducing the impact applied to the towline 102 after it has been separated.

【0003】例えば、特開平3−102200号では、
曳航索を繰り出すときに巻胴の回転を遅くさせるための
制動手段を設けるとともに、前記曳航索の外側端部を被
覆して保護することにより、前記曳航索の破断防止を図
った回転巻胴フィラメントディスペンサが提案されてい
る。
For example, in Japanese Patent Laid-Open No. 3-102200,
A rotating winding barrel filament designed to prevent breakage of the tow line by providing braking means for slowing the rotation of the tow line when the tow line is unwound and covering and protecting the outer end of the tow line. Dispensers have been proposed.

【0004】また、実開昭63−11299号では、曳
航索の繰り出し装置に電磁ブレーキを設け、この電磁ブ
レーキによって、繰り出し時における前記曳航索に加わ
る衝撃力を緩和することにより、前記曳航索の破断防止
を図った曳航装置が提案されている。
Further, in Japanese Utility Model Laid-Open No. 63-11299, an electromagnetic brake is provided in a towing line feeding device, and the electromagnetic brake reduces the impact force applied to the towing line at the time of feeding, thereby making the towing line move. A towing device designed to prevent breakage has been proposed.

【0005】さらに、実開昭63−11300号では、
上記実開昭63−11299号の曳航装置において、前
記曳航索と曳航標的(曳航体)の間に伸延性を有する緩
衝索を設け、前記曳航索の破断防止を図った曳航装置が
提案されている。
Furthermore, in Japanese Utility Model Publication No. 63-11300,
In the towing device of Japanese Utility Model Laid-Open No. 63-11299, a towing device has been proposed in which a tough line is provided between the towing line and a towing target (towing body) to prevent breakage of the towing line. There is.

【0006】[0006]

【発明が解決しようとする課題】ところが、これら従来
の曳航装置等では、母機から繰り出される曳航索に加わ
る衝撃力を緩和することはできるが、前記曳航体の曳航
中に、前記母機が旋回などの急激な軌道変化を行なった
際に、前記曳航索に加わる大きな張力を緩和することが
できなかった。
However, in these conventional towing devices, etc., the impact force applied to the tow line extended from the mother machine can be mitigated, but during the towing of the towed body, the mother machine turns or the like. It was not possible to relieve the large tension applied to the towline when the orbit was changed rapidly.

【0007】すなわち、従来の曳航体は、前記曳航索に
より前記母機に引かれるのみで自ら軌道変更することが
できなかった。このため、前記母機が急激な軌道変更を
行なうと、前記母機の運動に対して前記曳航体が遅れて
運動することとなり、このときの前記曳航体の空気抵抗
によって前記曳航索に大きな張力が加わり、前記曳航索
が破断してしまうという問題があった。
That is, the conventional towed body is not able to change its own trajectory only by being pulled by the mother aircraft by the tow line. For this reason, when the mother machine makes a sudden trajectory change, the towing body moves with a delay relative to the movement of the mother machine, and a large tension is applied to the tow line by the air resistance of the towing body at this time. However, there is a problem that the towline is broken.

【0008】また、前記母機が急激な軌道変更を行なう
と前記曳航索が破断してしまうので、前記母機の機動性
が制限され、これによって、前記曳航体の運動範囲も制
限されてしまうという問題もあった。
Further, when the mother machine makes a sudden change of the orbit, the tow line is broken, so that the maneuverability of the mother machine is limited, and thereby the range of motion of the towed body is also limited. There was also.

【0009】さらに、このような問題は、上記のように
母機によって曳航体を空中で曳航させる場合に限らず、
母船によって曳航体を水中で曳航させる場合でも同様に
生じる。
Further, such a problem is not limited to the case where the towing body is towed in the air by the mother machine as described above.
The same occurs when the towed body is towed underwater by the mother ship.

【0010】なお、特開昭57−196309号では、
曳航索にエレクトロメカニカルケーブルを用いることに
よって、母船と曳航体の有線式制御信号伝達系を形成
し、この有線式制御信号伝達系を介して前記曳航体を遠
隔制御する構成の曳航体の制御装置が提案されている。
Incidentally, in JP-A-57-196309,
By using an electromechanical cable for the tow line, a control system for a towed vehicle is formed, which forms a wired control signal transmission system between the mother ship and the towed vehicle, and remotely controls the towed vehicle via the wired control signal transmission system. Is proposed.

【0011】このような構成により、前記母船が軌道変
更した際に、前記母船の姿勢変化に追従させて前記曳航
体を素早く姿勢制御し、前記曳航索に大きな張力が加わ
るのを防止することも考えられる。しかし、この曳航体
の制御装置では、前記曳航体を姿勢制御するために特殊
なケーブルを必要とし、また、前記曳航体の姿勢制御
は、前記母船側において作業員が行なわなければなら
ず、前記母船の姿勢変化に追従させて前記曳航体を姿勢
制御することは現実的には非常に困難であった。
With such a structure, when the mother vessel changes its orbit, the attitude of the towed body can be quickly controlled by following the attitude change of the mother ship to prevent a large tension from being applied to the tow line. Conceivable. However, in this towed body control device, a special cable is required to control the attitude of the towed body, and the attitude control of the towed body must be performed by a worker on the mother ship side. In reality, it is very difficult to control the attitude of the towed body by following the attitude change of the mother ship.

【0012】本発明は、上記問題点にかんがみてなされ
たものであり、母機又は母船の姿勢変化に追従させて曳
航体を姿勢制御することを可能とし、これにより、曳航
索の破断事故の防止を図ることができるとともに、母機
又は母船の機動性の制限を緩和し、曳航体の運動範囲の
拡大を図ることができる曳航体の姿勢制御方法及び姿勢
制御装置の提供を目的とする。
The present invention has been made in view of the above problems, and makes it possible to control the attitude of a towed body by following the change in attitude of a mother machine or a mother ship, thereby preventing breakage accidents of the tow line. It is an object of the present invention to provide a posture control method and a posture control device for a towed body, which can alleviate restrictions on mobility of the mother machine or the mother ship and can expand the motion range of the towed body.

【0013】[0013]

【課題を解決するための手段】上記目的を達成するため
に、請求項1記載の曳航体の姿勢制御方法は、曳航索を
介して母機又は母船に曳航される曳航体の姿勢を制御す
る方法であって、前記曳航索に加わる張力の少なくとも
縦方向と横方向の成分にもとづいて、前記曳航体の姿勢
を制御することにより、前記曳航体の姿勢を前記母機又
は母船の姿勢変化に追従させる手順としてある。
In order to achieve the above object, the attitude control method for a towed vehicle according to claim 1, is a method for controlling the attitude of a towed vehicle towed by a mother aircraft or a mother ship via a tow line. The attitude of the towing body is controlled based on at least the longitudinal and lateral components of the tension applied to the towing line, so that the attitude of the towing body follows the attitude change of the mother machine or the mother ship. It is as a procedure.

【0014】また、このような方法を実施するため、請
求項2記載曳航体の姿勢制御装置は、曳航索を介して母
機又は母船に曳航される曳航体の姿勢を制御する装置で
あって、前記曳航索に加わる張力の縦方向及び横方向の
成分を検出する張力センサと、この張力センサが検出し
た前記曳航索の張力の縦方向及び横方向の成分にもとづ
いて、前記曳航体のピッチ制御量及びロール制御量を算
出する演算器と、この演算器の算出結果にもとづいて前
記曳航体の可動翼を駆動させる駆動部とを備えた構成と
してある。
In order to carry out such a method, the attitude control device for a towed vehicle according to claim 2 is a device for controlling the attitude of a towed vehicle towed by a mother machine or a mother ship via a tow line. A tension sensor for detecting vertical and horizontal components of tension applied to the tow line, and pitch control of the towed body based on the vertical and horizontal components of tension of the tow line detected by the tension sensor. It is configured to include an arithmetic unit that calculates the amount and the roll control amount, and a drive unit that drives the movable blade of the towed body based on the calculation result of the arithmetic unit.

【0015】このような本発明の曳航体の姿勢制御方法
及び姿勢制御装置によれば、前記母機又は母船の姿勢変
化に追従させて、前記曳航体の姿勢を制御することがで
きるので、前記母機又は母船の軌道変更時における前記
曳航体の空気抵抗を低減させることができる。
According to the attitude control method and attitude control device for a towed vehicle of the present invention, the attitude of the towed vehicle can be controlled by following the attitude change of the mother machine or the mother ship. Alternatively, it is possible to reduce the air resistance of the towed body when the trajectory of the mother ship is changed.

【0016】これにより、前記曳航索に加わる大きな張
力を減少させることができ、前記曳航索の破断事故を防
止することができる。この結果、前記母機又は母船の機
動性の制限が緩和され、前記曳航体の運動範囲を大幅に
拡大させることができる。また、曳航中の前記曳航体の
姿勢の乱れを自動的に修正することもできる。
As a result, a large tension applied to the tow line can be reduced and a breakage accident of the tow line can be prevented. As a result, the restriction on the maneuverability of the mother machine or the mother ship is relaxed, and the motion range of the towed body can be greatly expanded. Further, it is also possible to automatically correct the disturbance of the attitude of the towing body during towing.

【0017】[0017]

【発明の実施の形態】以下、本発明の曳航体の姿勢制御
方法及び姿勢制御装置の一実施形態について、図面を参
照しつつ説明する。図1は本発明の一実施形態に係る曳
航体の姿勢制御装置を示す説明図である。また、図2は
上記の姿勢制御装置の張力センサを示す斜視図であり、
図3は上記の姿勢制御装置のブロック図である。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of a towed vehicle attitude control method and attitude control apparatus according to the present invention will be described below with reference to the drawings. FIG. 1 is an explanatory diagram showing an attitude control device for a towed body according to an embodiment of the present invention. 2 is a perspective view showing a tension sensor of the above attitude control device,
FIG. 3 is a block diagram of the above attitude control device.

【0018】図1において、1は曳航体であり、曳航索
2を介して図示しない母機(航空機)に接続してある。
この曳航体1には、張力センサ11,制御演算器12及
び四つの駆動部13からなる姿勢制御装置が設けてあ
る。
In FIG. 1, reference numeral 1 is a towed vehicle, which is connected to a mother machine (aircraft) (not shown) via a tow line 2.
The towed body 1 is provided with an attitude control device including a tension sensor 11, a control calculator 12, and four drive units 13.

【0019】図1に示すように、張力センサ11には曳
航索2が結合してあり、張力センサ11は曳航索2に加
わる張力Fの、縦方向(Z軸方向)の成分FZ 及び横方
向(Y軸方向)の成分FY を検出する。
As shown in FIG. 1, the towline 2 is coupled to the tension sensor 11, and the tension sensor 11 is arranged to measure the component F Z of the tension F applied to the towline 2 in the longitudinal direction (Z-axis direction) and the lateral direction. The component F Y in the direction (Y-axis direction) is detected.

【0020】この張力センサ11は、例えば、図2に示
すように、曳航体1のX,Y,Z軸方向にそれぞれ突出
する軸部を有する支持金具11aと、この支持金具11
のY軸方向及びZ軸方向に突出する二つの軸部にそれぞ
れ取り付けた歪みゲージ11bとによって形成すること
ができる。
The tension sensor 11 is, for example, as shown in FIG. 2, a support fitting 11a having shaft portions projecting in the X-, Y-, and Z-axis directions of the towed body 1, and the support fitting 11 respectively.
Can be formed by the strain gauges 11b respectively attached to the two shaft portions protruding in the Y-axis direction and the Z-axis direction.

【0021】このような構成によれば、曳航索2に張力
Fが加わると、支持金具11aを形成する各軸部に微小
な歪みが生じ、この歪みを各歪みゲージ11bによって
検出することにより、曳航索2に加わる張力Fの、縦方
向の成分FZ 及び横方向の成分FY を検出することがで
きる。
With such a structure, when tension F is applied to the towline 2, a minute strain is generated in each shaft portion forming the support fitting 11a, and this strain is detected by each strain gauge 11b. It is possible to detect the vertical component F Z and the horizontal component F Y of the tension F applied to the towline 2.

【0022】制御演算器12は、図3に示すように、ピ
ッチ制御部12aとロール制御部12bを有する。ピッ
チ制御部12aは、張力センサ11からの縦方向の成分
Z を入力し、曳航体1の縦方向の制御量を算出する。
また、ロール制御部12bは、張力センサ11からの横
方向の成分FY を入力し、曳航体1の横方向の制御量を
算出する。
As shown in FIG. 3, the control calculator 12 has a pitch controller 12a and a roll controller 12b. The pitch control unit 12a inputs the vertical component F Z from the tension sensor 11 and calculates the vertical control amount of the towed vehicle 1.
Further, the roll control unit 12b inputs the lateral component F Y from the tension sensor 11 and calculates the lateral control amount of the towing vehicle 1.

【0023】ここで、図4はこれらピッチ制御部12a
及びロール制御部12bを示すブロック図であり、同図
を参照しつつ、これらピッチ制御部12a及びロール制
御部12bについて説明する。なお、これらピッチ制御
部12a及びロール制御部12bは、制御する方向(縦
方向と横方向)が異なるのみで、その構成はほぼ同じと
なっている。
Here, FIG. 4 shows these pitch control sections 12a.
FIG. 3 is a block diagram showing a roll control unit 12b and a roll control unit 12b. The pitch control unit 12a and the roll control unit 12b will be described with reference to FIG. The pitch control unit 12a and the roll control unit 12b are substantially the same in configuration except that they are controlled in different directions (vertical direction and horizontal direction).

【0024】同図において、縦方向の成分FZ (又は横
方向の成分FY )を入力したピッチ制御部12a(又は
ロール制御部12b)は、一方で、 (1)この縦方向の成分FZ を最終目標量0と比較して
誤差量S0 を算出する。 (2)この誤差量S0 を比例定数部121に入力し、誤
差に比例した制御量S1を算出する。 (3)また、このとき、誤差量S0 を積分器122及び
比例定数部123に入力し、誤差の積分量に比例した制
御量S2 を算出する。
In the figure, the pitch control section 12a (or the roll control section 12b) to which the vertical component F Z (or the horizontal component F Y ) is input is, on the other hand, (1) The vertical component F Z The error amount S 0 is calculated by comparing Z with the final target amount 0. (2) This error amount S 0 is input to the proportional constant unit 121, and the control amount S 1 proportional to the error is calculated. (3) At this time, the error amount S 0 is input to the integrator 122 and the proportional constant unit 123, and the control amount S 2 proportional to the error integration amount is calculated.

【0025】(4)さらに、ピッチ制御部12aは、他
方で、縦方向の成分FZ を微分器124及び比例定数部
125に入力し、誤差の微分、すなわち、変化量に比例
した制御量S3 を算出する。 (5)その後、誤差に比例した制御量S1 ,誤差の積分
量に比例した制御量S2,変化量に比例した制御量S3
を加算して(S4 )、この算出結果S4 を比例定数部1
26に入力し、最終制御量S5 を算出する。
(4) Further, the pitch control unit 12a, on the other hand, inputs the vertical component F Z to the differentiator 124 and the proportional constant unit 125, and differentiates the error, that is, the control amount S proportional to the change amount. Calculate 3 . (5) After that, the control amount S 1 proportional to the error, the control amount S 2 proportional to the integral amount of the error, and the control amount S 3 proportional to the change amount.
Is added (S 4 ), and this calculation result S 4 is added to the proportional constant part 1
26, and the final controlled variable S 5 is calculated.

【0026】各駆動部13は、図1に示すように、曳航
体1の後端部に取り付けた四枚の可動翼1aにそれぞれ
接続してあり、図2に示すように、ピッチ制御部12a
及びロール制御部12bから出力された最終制御量S5
にもとづいて四枚の可動翼1aを回動させる。これによ
り、前記母機の姿勢変化に追従して曳航体1の姿勢が制
御される。
As shown in FIG. 1, each drive unit 13 is connected to four movable blades 1a attached to the rear end of the towing body 1, and as shown in FIG. 2, a pitch control unit 12a.
And the final control amount S 5 output from the roll controller 12b
Based on this, the four movable wings 1a are rotated. As a result, the attitude of the towed body 1 is controlled by following the attitude change of the mother machine.

【0027】このような本実施形態の曳航体の姿勢制御
方法及び姿勢制御装置によれば、前記母機の姿勢変化に
追従させて、曳航体1の姿勢を制御することができるの
で、前記母機の軌道変更時における曳航体1の空気抵抗
を低減させることができる。
According to the attitude control method and the attitude control device for a towed vehicle of the present embodiment, the attitude of the towed vehicle 1 can be controlled by following the attitude change of the mother machine. It is possible to reduce the air resistance of the towed body 1 when the trajectory is changed.

【0028】これにより、曳航索2に加わる大きな張力
を減少させることができ、曳航索2の破断事故を防止す
ることができる。この結果、前記母機の機動性の制限が
緩和され、曳航体1の運動範囲を大幅に拡大させること
ができる。また、曳航中の曳航体1の姿勢の乱れを自動
的に修正することもできる。
As a result, a large tension applied to the towline 2 can be reduced and a breakage accident of the towline 2 can be prevented. As a result, the restriction on the maneuverability of the mother machine is relaxed, and the range of motion of the towed body 1 can be greatly expanded. Further, it is also possible to automatically correct the attitude disorder of the towing body 1 during towing.

【0029】なお、本発明の曳航体の姿勢制御方法及び
姿勢制御装置は、上述した実施形態に限定されるもので
はない。例えば、本発明の曳航体の姿勢制御方法及び姿
勢制御装置は、上記のように母機によって曳航体を空中
で曳航させる場合に限らず、母船によって曳航体を水中
で曳航させる場合にも応用することができる。
The attitude control method and attitude control device for a towed body of the present invention are not limited to the above-described embodiments. For example, the attitude control method and attitude control device of the towed body of the present invention are not limited to the case where the towing body is towed in the air by the mother machine as described above, and may be applied to the case where the towing body is towed underwater by the mother ship. You can

【0030】また、上述した本実施例の姿勢制御装置で
は、曳航体1の姿勢制御を簡単に行なうという観点か
ら、張力Fを形成する成分のうち、縦方向の成分FZ
び横方向の成分FY のみにもとづいて曳航体1の姿勢を
制御する構成としたが、これら成分FZ 及びFY に曳航
方向(X軸方向)の成分FX を加えて曳航体1の姿勢を
制御する構成とすることもできる。
Further, in the attitude control device of the present embodiment described above, from the viewpoint of simply performing the attitude control of the towed body 1, of the components forming the tension F, the vertical component F Z and the horizontal component. Although the configuration of controlling the attitude of the towing vehicle 1 is based only on F Y , the attitude of the towing vehicle 1 is controlled by adding the component F X in the towing direction (X-axis direction) to these components F Z and F Y. Can also be

【0031】すなわち、図2に示すように、張力センサ
11の支持金具11aのX軸方向に突出する軸部に歪み
ゲージ(二点鎖線)を追加し、この歪みゲージによって
検知したX軸方向の成分FX を、図3及び図4における
ロール制御量及びピッチ制御量の演算に加えれば、X,
Y,Z軸方向の成分FX ,FY ,FZ にもとづいて曳航
体1の姿勢を制御することができる。
That is, as shown in FIG. 2, a strain gauge (two-dot chain line) is added to the shaft portion of the support fitting 11a of the tension sensor 11 projecting in the X-axis direction, and the strain gauge detects the X-axis direction. If the component F X is added to the calculation of the roll control amount and the pitch control amount in FIGS. 3 and 4, X,
The attitude of the towed vehicle 1 can be controlled based on the components F X , F Y , and F Z in the Y and Z axis directions.

【0032】[0032]

【発明の効果】以上のように、本発明の曳航体の姿勢制
御方法及び姿勢制御装置によれば、母機又は母船の姿勢
変化に追従させて曳航体を姿勢制御することを可能と
し、これにより、曳航索の破断事故の防止を図ることが
できるとともに、母機又は母船の機動性の制限を緩和
し、曳航体の運動範囲の拡大を図ることができる。
As described above, according to the attitude control method and attitude control device for a towed vehicle of the present invention, it is possible to control the attitude of the towed vehicle by following the attitude change of the mother aircraft or the mother ship. It is possible to prevent breakage accidents of the towline, relax the mobility limitation of the mother machine or the mother ship, and expand the range of motion of the towed body.

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

【図1】本発明の一実施形態に係る曳航体の姿勢制御装
置を示す説明図である。
FIG. 1 is an explanatory diagram showing an attitude control device for a towed body according to an embodiment of the present invention.

【図2】上記の姿勢制御装置の張力センサを示す斜視図
である。
FIG. 2 is a perspective view showing a tension sensor of the attitude control device.

【図3】上記の姿勢制御装置のブロック図である。FIG. 3 is a block diagram of the attitude control device.

【図4】上記の姿勢制御装置の制御演算部を形成するピ
ッチ制御部及びロール制御部を示すブロック図である。
FIG. 4 is a block diagram showing a pitch control unit and a roll control unit that form a control calculation unit of the attitude control device.

【図5】母機(航空機)により曳航体を曳航している状
態を示す斜視図である。
FIG. 5 is a perspective view showing a state in which a towing body is towed by a mother aircraft (aircraft).

【符号の説明】[Explanation of symbols]

1 曳航体 2 曳航索 11 張力センサ 12 制御演算部 12a ピッチ制御部 12b ロール制御部 121,123,125,126 比例定数部 122 積分器 124 微分器 DESCRIPTION OF SYMBOLS 1 Towing body 2 Towing line 11 Tension sensor 12 Control calculation part 12a Pitch control part 12b Roll control part 121,123,125,126 Proportional constant part 122 Integrator 124 Differentiator

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 曳航索を介して母機又は母船に曳航され
る曳航体の姿勢を制御する方法であって、 前記曳航索に加わる張力の少なくとも縦方向と横方向の
成分にもとづいて、前記曳航体の姿勢を制御することに
より、前記曳航体の姿勢を前記母機又は母船の姿勢変化
に追従させることを特徴とする曳航体の姿勢制御方法。
1. A method of controlling the attitude of a towed body towed by a mother aircraft or a mother ship via a towline, wherein the towline is based on at least a longitudinal component and a lateral component of a tension applied to the towline. A towed body attitude control method, wherein the attitude of the towed body is made to follow the attitude change of the mother machine or the mother ship by controlling the body attitude.
【請求項2】 曳航索を介して母機又は母船に曳航され
る曳航体の姿勢を制御する装置であって、 前記曳航索に加わる張力の縦方向及び横方向の成分を検
出する張力センサと、 この張力センサが検出した前記曳航索の張力の縦方向及
び横方向の成分にもとづいて、前記曳航体のピッチ制御
量及びロール制御量を算出する演算器と、 この演算器の算出結果にもとづいて前記曳航体の可動翼
を駆動させる駆動部とを備えたことを特徴とする曳航体
の姿勢制御装置。
2. A device for controlling the attitude of a towed body towed by a mother machine or a mother ship via a tow line, comprising a tension sensor for detecting longitudinal and lateral components of tension applied to the tow line. An arithmetic unit for calculating the pitch control amount and roll control amount of the towed body based on the longitudinal and lateral components of the tension of the tow line detected by the tension sensor, and based on the calculation result of this arithmetic unit. An attitude control device for a towed body, comprising: a drive unit that drives a movable blade of the towed body.
JP7320603A 1995-12-08 1995-12-08 Attitude control method and attitude control device for towed body Expired - Lifetime JP2682525B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7320603A JP2682525B2 (en) 1995-12-08 1995-12-08 Attitude control method and attitude control device for towed body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7320603A JP2682525B2 (en) 1995-12-08 1995-12-08 Attitude control method and attitude control device for towed body

Publications (2)

Publication Number Publication Date
JPH09159397A true JPH09159397A (en) 1997-06-20
JP2682525B2 JP2682525B2 (en) 1997-11-26

Family

ID=18123259

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7320603A Expired - Lifetime JP2682525B2 (en) 1995-12-08 1995-12-08 Attitude control method and attitude control device for towed body

Country Status (1)

Country Link
JP (1) JP2682525B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015117586A1 (en) * 2014-02-07 2015-08-13 Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung Towed active flying object for collecting measurement data

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2015117586A1 (en) * 2014-02-07 2015-08-13 Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung Towed active flying object for collecting measurement data
US9714092B2 (en) 2014-02-07 2017-07-25 Alfred-Wegener-Institut Helmholtzzentrum Fuer Polar- Und Meeresforschung Towed active airborne platform for determining measurement data

Also Published As

Publication number Publication date
JP2682525B2 (en) 1997-11-26

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