JPS61110111U - - Google Patents
Info
- Publication number
- JPS61110111U JPS61110111U JP20030984U JP20030984U JPS61110111U JP S61110111 U JPS61110111 U JP S61110111U JP 20030984 U JP20030984 U JP 20030984U JP 20030984 U JP20030984 U JP 20030984U JP S61110111 U JPS61110111 U JP S61110111U
- Authority
- JP
- Japan
- Prior art keywords
- gyro
- calculator
- torque
- power amplifier
- power
- 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
- 241000597000 Freesia Species 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Description
第1図はこの考案の一実施例を示す構成図、第
2図は従来のフリージヤイロ装置による追尾装置
を示す構成図である。
図において、1はジヤイロロータ、2,3,4
は各々右手直交系のx軸y軸z軸、5はジヤイロ
ロータスピン軸、6は内部ジンバル、7は外部ジ
ンバル、8は機体、9,10は第1のトルク発生
器、11,12はベアリング、13は信号検出器
、14は角度検出器、15は第1の計算器、16
は第1の電力増幅器、17,18は第2のトルク
発生器、19,20は角速度検出器、21は第2
の計算器、22は第2の電力増幅器である。なお
、各図中同一符号は同一または相当部分を示す。
FIG. 1 is a block diagram showing an embodiment of this invention, and FIG. 2 is a block diagram showing a tracking device using a conventional free-gear gyro device. In the figure, 1 is a gyro rotor, 2, 3, 4
are the x-axis, y-axis, and z-axis of the right-handed orthogonal system, 5 is the gyro rotor spin axis, 6 is the internal gimbal, 7 is the external gimbal, 8 is the aircraft body, 9 and 10 are the first torque generators, and 11 and 12 are the Bearing, 13 is a signal detector, 14 is an angle detector, 15 is a first calculator, 16
is the first power amplifier, 17 and 18 are the second torque generators, 19 and 20 are the angular velocity detectors, and 21 is the second
22 is a second power amplifier. Note that the same reference numerals in each figure indicate the same or corresponding parts.
Claims (1)
ジヤイロ、このフリージヤイロのジヤイロロータ
上の信号検出器、その信号検出器と目標物体とを
結ぶ目視線とジヤイロロータスピン軸とのなす角
、いわゆるボアサイト角を検出する角度検出器、
このボアサイト角が零になる様なプリセツシヨン
を発生するジヤイロロータへのトルクを計算する
第1の計算器、この計算器の出力を受けて電力増
幅する第1の電力増幅器、この電力増幅器によつ
て駆動されジヤイロロータに実際にトルクを加え
る第1のトルク発生器、さらに機体とフリージヤ
イロのジンバルの相対角速度あるいはジンバルど
うしの相対角速度を検出する角速度検出器、検出
器の出力を受けてこの角速度によつて生じる外乱
トルクを計算する計算器、この計算器の出力を受
けて電力増幅する第2の電力増幅器、この電力増
幅器によつて駆動されジヤイロロータに実際にト
ルクを加える第2のトルク発生器を備えたことを
特徴とするフリージヤイロ装置。 A free-gear gyro mounted on an aircraft that oscillates in inertial space, a signal detector on the gyro rotor of this free-gear gyro, and an angle between the line of sight connecting the signal detector and the target object and the gyro rotor spin axis, the so-called boresight angle. Angle detector to detect,
A first calculator that calculates the torque to the gyro rotor that generates a preset such that the boresight angle becomes zero, a first power amplifier that amplifies the power in response to the output of this calculator, and a first power amplifier that amplifies the power by receiving the output of this calculator. A first torque generator that is driven and actually applies torque to the gyro rotor; an angular velocity detector that detects the relative angular velocity between the gimbals of the aircraft and the free gyro, or the relative angular velocity between the gimbals; It includes a calculator that calculates the disturbance torque that occurs, a second power amplifier that receives the output of this calculator and amplifies the power, and a second torque generator that is driven by the power amplifier and actually applies torque to the gyro rotor. A freesia gyro device characterized by:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20030984U JPS61110111U (en) | 1984-12-25 | 1984-12-25 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20030984U JPS61110111U (en) | 1984-12-25 | 1984-12-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS61110111U true JPS61110111U (en) | 1986-07-12 |
Family
ID=30761036
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP20030984U Pending JPS61110111U (en) | 1984-12-25 | 1984-12-25 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS61110111U (en) |
-
1984
- 1984-12-25 JP JP20030984U patent/JPS61110111U/ja active Pending
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4321678A (en) | Apparatus for the automatic determination of a vehicle position | |
CA1141008A (en) | Autonomous navigation system | |
US5369889A (en) | Single gyro northfinder | |
US4052654A (en) | Gyro stabilized inertial reference system with gimbal lock prevention means | |
JPS61110111U (en) | ||
US3140482A (en) | System providing error rate damping of an autonavigator | |
JPH02243917A (en) | Compass system | |
US5064285A (en) | Position-controlled electromagnetic assembly | |
CA1325903C (en) | Gyroscope system | |
GB1149164A (en) | A viewing device | |
US3898744A (en) | Constant precessed gyrocompass | |
US3762062A (en) | Twin gyro north seeker | |
JP2770076B2 (en) | Late bias device | |
US5065956A (en) | Method for detecting changes in spin rate of a missile in flight | |
JPH0131568B2 (en) | ||
JPS6374995U (en) | ||
JP3118058B2 (en) | Speed detector | |
JPS6032565Y2 (en) | Free-gyro gimbal drive device | |
GB1509293A (en) | Instruments for measuring the orientation of a borehole | |
RU2047093C1 (en) | Gyroplatform stabilized in horizon plane | |
JPH0861956A (en) | Azimuth sensor | |
SU146057A1 (en) | Sensitive element of the autonomous control system | |
JPH04142087A (en) | Rate biasing device | |
JPS60193799A (en) | Controller for attitude and antenna directivity of artificial satellite | |
JPS58186808A (en) | Guidance system of airframe |