JPS6323598U - - Google Patents
Info
- Publication number
- JPS6323598U JPS6323598U JP11576586U JP11576586U JPS6323598U JP S6323598 U JPS6323598 U JP S6323598U JP 11576586 U JP11576586 U JP 11576586U JP 11576586 U JP11576586 U JP 11576586U JP S6323598 U JPS6323598 U JP S6323598U
- Authority
- JP
- Japan
- Prior art keywords
- output
- steering
- controller
- transfer function
- input
- 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
- 230000001133 acceleration Effects 0.000 claims description 2
- 230000005540 biological transmission Effects 0.000 claims description 2
- 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概略構成ブ
ロツク図、第2図は従来の飛しよう体のピツチ系
またはヨー系オートパイロツトの概略構成ブロツ
ク図であり、図中1は加速度コマンド、2はコン
トローラ、3はピツチ系またはヨー系の舵角指令
信号、4は操舵サーボ装置、5は舵角、6は機体
伝達特性、7はピツチ系またはヨー系の角速度及
び加速度、8は慣性センサ、9は慣性センサ出力
、10は可変パラメータコントローラ、11は機
体伝達関数パラメータ同定器、12はコントロー
ラパラメータ計算器である。なお、図中同一ある
いは相当部分には同一符号を付して示してある。
Fig. 1 is a schematic block diagram showing an embodiment of this invention, and Fig. 2 is a schematic block diagram of a conventional pitch or yaw autopilot for flying vehicles. is a controller, 3 is a pitch or yaw system steering angle command signal, 4 is a steering servo device, 5 is a steering angle, 6 is an airframe transmission characteristic, 7 is a pitch or yaw system angular velocity and acceleration, 8 is an inertial sensor, 9 is an inertial sensor output, 10 is a variable parameter controller, 11 is an aircraft transfer function parameter identifier, and 12 is a controller parameter calculator. It should be noted that the same or corresponding parts in the figures are indicated by the same reference numerals.
Claims (1)
イロツト装置において、所望の特性となる様に制
御補償を行うパラメータ可変コントローラと、上
記コントローラの出力の舵角指令信号を入力とし
て操舵翼を上記舵角指令信号と同じ大きさの舵角
となる様に制御する操舵サーボ装置と、上記操舵
サーボ装置出力の一端の舵角を入力とする飛しよ
う体伝達特性を有する出力をもとに飛しよう体の
ピツチ系またはヨー系の角速度及び加速度を検出
する慣性センサと、上記操舵サーボ装置出力の他
端と上記慣性センサの出力を入力として機体の伝
達関数パラメータを実時間で同定する機体伝達関
数パラメータ同定器と、上記同定器で同定された
機体伝達関数パラメータをもとに計算するコント
ローラパラメータ計算器とによつて閉ループを構
成することを特徴とする飛しよう体のオートパイ
ロツト装置。 In a pitch system or yaw system autopilot system for a flying object, there is a variable parameter controller that performs control compensation to achieve desired characteristics, and a rudder angle command signal output from the controller is input to control the steering blades according to the rudder angle command. A steering servo device that controls the steering angle so that it has the same magnitude as the signal, and a pitch of the flying object based on an output having a flying object transmission characteristic using the steering angle of one end of the output of the above-mentioned steering servo device as input. an inertial sensor that detects the angular velocity and acceleration of the system or the yaw system, and an aircraft transfer function parameter identifier that identifies the aircraft transfer function parameter in real time using the other end of the output of the steering servo device and the output of the inertial sensor as input. , and a controller parameter calculator that calculates based on the aircraft transfer function parameters identified by the above-described identifier, forming a closed loop.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11576586U JPS6323598U (en) | 1986-07-28 | 1986-07-28 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11576586U JPS6323598U (en) | 1986-07-28 | 1986-07-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6323598U true JPS6323598U (en) | 1988-02-16 |
Family
ID=30999727
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP11576586U Pending JPS6323598U (en) | 1986-07-28 | 1986-07-28 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6323598U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02143098A (en) * | 1988-11-25 | 1990-06-01 | Tech Res & Dev Inst Of Japan Def Agency | Roll controller for fore wing steering missile |
-
1986
- 1986-07-28 JP JP11576586U patent/JPS6323598U/ja active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02143098A (en) * | 1988-11-25 | 1990-06-01 | Tech Res & Dev Inst Of Japan Def Agency | Roll controller for fore wing steering missile |
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