JPS56143014A - Inducing device of flying body - Google Patents

Inducing device of flying body

Info

Publication number
JPS56143014A
JPS56143014A JP4620380A JP4620380A JPS56143014A JP S56143014 A JPS56143014 A JP S56143014A JP 4620380 A JP4620380 A JP 4620380A JP 4620380 A JP4620380 A JP 4620380A JP S56143014 A JPS56143014 A JP S56143014A
Authority
JP
Japan
Prior art keywords
flying body
angular speed
gain
attitude angular
automatic gain
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
JP4620380A
Other languages
Japanese (ja)
Other versions
JPH0230044B2 (en
Inventor
Yuzo Katayama
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.)
Toshiba Corp
Original Assignee
Toshiba Corp
Tokyo Shibaura Electric Co Ltd
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 Toshiba Corp, Tokyo Shibaura Electric Co Ltd filed Critical Toshiba Corp
Priority to JP4620380A priority Critical patent/JPS56143014A/en
Publication of JPS56143014A publication Critical patent/JPS56143014A/en
Publication of JPH0230044B2 publication Critical patent/JPH0230044B2/ja
Granted 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

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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

PURPOSE:To enable to suppress the excessive movement of an induced flying body, by automatically decreasing the gain of the induction control system when the amplitude of the specific frequency component other than the homing signal among steering signals reaches a high level. CONSTITUTION:The output signal of a homing device 11 is fed to the steering device 13 via the automatic gain adjuster 31. The attitude angular speed of the movement of a flying body 14 is detected with the rate gyroscope 15, the average value of the absolute value is made with the angular speed average circuit 32, and the gain of the induced control system is automatically adjusted with said average value by means of the automatic gain adjuster 31. That is, the gain of the automatic gain adjuster 31 is taken as the normal gain until the attitude angular speed of the induced flying body 14 reaches a set level, and when the attitude angular speed of a flying body 14 is increased in excess of the set level, the gain of the automatic gain adjuster 31 is automatically decreased. Thus, excessive attitude angular speed can be suppressed normally to the flying body 14.
JP4620380A 1980-04-10 1980-04-10 Inducing device of flying body Granted JPS56143014A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4620380A JPS56143014A (en) 1980-04-10 1980-04-10 Inducing device of flying body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4620380A JPS56143014A (en) 1980-04-10 1980-04-10 Inducing device of flying body

Publications (2)

Publication Number Publication Date
JPS56143014A true JPS56143014A (en) 1981-11-07
JPH0230044B2 JPH0230044B2 (en) 1990-07-04

Family

ID=12740518

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4620380A Granted JPS56143014A (en) 1980-04-10 1980-04-10 Inducing device of flying body

Country Status (1)

Country Link
JP (1) JPS56143014A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2604517A1 (en) * 1986-09-26 1988-04-01 Borg Instr Gmbh ARRANGEMENT FOR DETERMINING AN AVERAGE VALUE

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52147893A (en) * 1976-06-04 1977-12-08 Tokyo Keiki Co Ltd Automatic steering method for ship
JPS5494800A (en) * 1978-01-09 1979-07-26 Nec Corp Searching and tracing device

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52147893A (en) * 1976-06-04 1977-12-08 Tokyo Keiki Co Ltd Automatic steering method for ship
JPS5494800A (en) * 1978-01-09 1979-07-26 Nec Corp Searching and tracing device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2604517A1 (en) * 1986-09-26 1988-04-01 Borg Instr Gmbh ARRANGEMENT FOR DETERMINING AN AVERAGE VALUE

Also Published As

Publication number Publication date
JPH0230044B2 (en) 1990-07-04

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