JPS6164100U - - Google Patents

Info

Publication number
JPS6164100U
JPS6164100U JP1985149911U JP14991185U JPS6164100U JP S6164100 U JPS6164100 U JP S6164100U JP 1985149911 U JP1985149911 U JP 1985149911U JP 14991185 U JP14991185 U JP 14991185U JP S6164100 U JPS6164100 U JP S6164100U
Authority
JP
Japan
Prior art keywords
flying object
operational amplifier
control signal
control
field effect
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
JP1985149911U
Other languages
Japanese (ja)
Other versions
JPS6222480Y2 (en
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 filed Critical
Publication of JPS6164100U publication Critical patent/JPS6164100U/ja
Application granted granted Critical
Publication of JPS6222480Y2 publication Critical patent/JPS6222480Y2/ja
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Transmitters (AREA)
  • Pens And Brushes (AREA)

Description

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

第１図は、飛行物体の垂直および水平方向の誘
導チヤンネルを有する誘導装置を示すブロツク線
図であり、第２図は、ノツチ・フイルタの好まし
い実施例を示す回路図である。 １はコンピユータ、２，４は信号処理装置、３
，５はノツチ・フイルタ、６は操縦面サーボ、７
は制御入力、８は操作入力、９は出力、１０は演
算増幅器である。 1 is a block diagram illustrating a guidance system with vertical and horizontal guidance channels for a flying object, and FIG. 2 is a circuit diagram illustrating a preferred embodiment of a notch filter. 1 is a computer, 2 and 4 are signal processing devices, 3
, 5 is a notch filter, 6 is a control surface servo, 7
is a control input, 8 is an operation input, 9 is an output, and 10 is an operational amplifier.

Claims (1)

【実用新案登録請求の範囲】 １ 誤差信号を飛行物体の操縦面サーボに対する
指令信号に変換するための誘導チヤンネルを少な
くとも一つ有する飛行物体の誘導装置において、 固有振動数が飛行物体の速度の関数として変化
する飛行物体の固有振動数での狭い帯域で前記チ
ヤンネルにおいて振動を減衰させる装置を具備し
、この振動減衰装置は、前記チヤンネルにおける
ノツチ・フイルタを含み、このノツチ・フイルタ
は制御可能なノツチ周波数を有し、およびこのノ
ツチ・フイルタのノツチ周波数を飛行物体の固有
振動数に一致させるべく制御する装置を含み、飛
行物体の速度で変化する制御信号Ｕｖを与える装
置を具備し、この制御信号Ｕｖは前記ノツチ周波
数を制御すべく前記ノツチ・フイルタの制御入力
に接続されていることを特徴とする飛行物体の誘
導装置。 ２ 前記制御信号は飛行物体の縦方向加速および
減速を測定する加速度計からの信号を積分して得
られるものである実用新案登録請求の範囲第１項
記載の飛行物体の誘導装置。 ３ 前記ノツチ・フイルタは演算増幅器１０と帰
還枝路とからなり、前記飛行物体の制御信号は、
分圧器Ｒ２，Ｒ３を介して前記演算増幅器の正側
入力に供給され、かつ抵抗Ｒ１と直列の蓄電池Ｃ
１を介して前記演算増幅器の負側入力に供給され
るようになされており、前記帰還枝路は前記演算
増幅器とその負側入力との間に接続された抵抗Ｒ
０と並列の蓄電器Ｃ０からなる実用新案登録請求
の範囲第２項記載の飛行物体の誘導装置。 ４ 前記演算増幅器の前記負側入力と前記帰還枝
路との接続部の双方に電界効果トランジスター（
それぞれＱ１およびＱ２）を設け、これら電界効
果トランジスターが前記速度に依存する前記制御
信号Ｕｖにより制御される実用新案登録請求の範
囲第３項記載の飛行物体の誘導装置。[Claims for Utility Model Registration] 1. In a guidance device for a flying object having at least one guidance channel for converting an error signal into a command signal for a control surface servo of the flying object, the natural frequency is a function of the speed of the flying object. a device for damping vibrations in said channel in a narrow band at the natural frequency of the flying object varying as and a device for controlling the notch frequency of the notch filter to match the natural frequency of the flying object, and a device for providing a control signal Uv varying with the speed of the flying object; 2. A system for guiding a flying object, characterized in that Uv is connected to a control input of the notch filter to control the notch frequency. 2. The flying object guidance device according to claim 1, wherein the control signal is obtained by integrating signals from an accelerometer that measures longitudinal acceleration and deceleration of the flying object. 3. The notch filter consists of an operational amplifier 10 and a return branch, and the control signal for the flying object is
A storage battery C is supplied to the positive input of the operational amplifier via a voltage divider R 2 , R 3 and is in series with a resistor R 1 .
1 to the negative input of the operational amplifier, and the feedback branch is connected to a resistor R connected between the operational amplifier and its negative input.
2. A guidance device for a flying object according to claim 2, which comprises a capacitor C0 in parallel with C0 . 4 A field effect transistor (
4. The flying object guidance device according to claim 3, wherein field effect transistors Q 1 and Q 2 ) are provided, and these field effect transistors are controlled by the control signal Uv that depends on the speed.
JP1985149911U 1975-01-14 1985-09-30 Expired JPS6222480Y2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7500342A SE396473B (en) 1975-01-14 1975-01-14 DEVICE FOR DAMPING OF TIP AND GEAR SWITCHES

Publications (2)

Publication Number Publication Date
JPS6164100U true JPS6164100U (en) 1986-05-01
JPS6222480Y2 JPS6222480Y2 (en) 1987-06-08

Family

ID=20323396

Family Applications (2)

Application Number Title Priority Date Filing Date
JP51003726A Pending JPS5195400A (en) 1975-01-14 1976-01-13
JP1985149911U Expired JPS6222480Y2 (en) 1975-01-14 1985-09-30

Family Applications Before (1)

Application Number Title Priority Date Filing Date
JP51003726A Pending JPS5195400A (en) 1975-01-14 1976-01-13

Country Status (9)

Country Link
JP (2) JPS5195400A (en)
CH (1) CH601767A5 (en)
DE (1) DE2600532C2 (en)
FR (1) FR2298132A1 (en)
GB (1) GB1533011A (en)
IT (1) IT1052918B (en)
NL (1) NL7600074A (en)
NO (1) NO145215C (en)
SE (1) SE396473B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003051552A1 (en) * 2001-12-19 2003-06-26 Showa Denko K.K. Extrusion tool, method for manufacturing shaped article with fins, and heat sink

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3037673C2 (en) * 1980-10-04 1983-12-08 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Drive device for controlling the rudder of a missile with a servomotor
US5072893A (en) * 1987-05-28 1991-12-17 The Boeing Company Aircraft modal suppression system
FR2672028B1 (en) * 1991-01-29 1993-05-14 Aerospatiale SYSTEM FOR IMPROVING THE FLOATING BEHAVIOR OF AN AIRCRAFT.

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4853500A (en) * 1971-11-08 1973-07-27

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3331951A (en) * 1963-02-20 1967-07-18 James E Webb Trigonometric vehicle guidance assembly which aligns the three perpendicular axes of two three-axes systems
DE1239200B (en) * 1964-03-05 1967-04-20 Bodenseewerk Perkin Elmer Co Damping device for flight control systems for unmanned aerial vehicles
DE2165894C2 (en) * 1971-12-31 1983-01-20 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Arrangement for controlling and stabilizing an aircraft

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4853500A (en) * 1971-11-08 1973-07-27

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003051552A1 (en) * 2001-12-19 2003-06-26 Showa Denko K.K. Extrusion tool, method for manufacturing shaped article with fins, and heat sink
CN1292853C (en) * 2001-12-19 2007-01-03 昭和电工株式会社 Extrusion tool, method for manufacturing shaped article with fins, and heat sink

Also Published As

Publication number Publication date
GB1533011A (en) 1978-11-22
FR2298132B1 (en) 1982-04-23
NO145215B (en) 1981-10-26
CH601767A5 (en) 1978-07-14
JPS6222480Y2 (en) 1987-06-08
IT1052918B (en) 1981-08-31
SE396473B (en) 1977-09-19
NL7600074A (en) 1976-07-16
FR2298132A1 (en) 1976-08-13
NO145215C (en) 1982-02-10
SE7500342L (en) 1976-07-15
JPS5195400A (en) 1976-08-20
DE2600532A1 (en) 1976-07-15
NO760032L (en) 1976-07-15
DE2600532C2 (en) 1987-03-19

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