JPS5791434A - Simulator of load on steering wing - Google Patents

Simulator of load on steering wing

Info

Publication number
JPS5791434A
JPS5791434A JP55167543A JP16754380A JPS5791434A JP S5791434 A JPS5791434 A JP S5791434A JP 55167543 A JP55167543 A JP 55167543A JP 16754380 A JP16754380 A JP 16754380A JP S5791434 A JPS5791434 A JP S5791434A
Authority
JP
Japan
Prior art keywords
steering
load
output
steering angle
missile
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
Application number
JP55167543A
Other languages
Japanese (ja)
Inventor
Kaoru Tanaka
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
Nippon 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 NEC Corp, Nippon Electric Co Ltd filed Critical NEC Corp
Priority to JP55167543A priority Critical patent/JPS5791434A/en
Publication of JPS5791434A publication Critical patent/JPS5791434A/en
Pending 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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/02—Control of position or course in two dimensions

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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

PURPOSE:To apply load torque to a steering wing automatically by multiplying a signal which is in proportion to the square of a speed from a computer by the output of a steering angle detector which detects a steering angle at a multiplier, and using the result of the multiplication. CONSTITUTION:Simulation is so performed that a steering wing load which is in proportion to the square of the speed of a missile or underwater running body in addition to a steering angle is applied to the steering wing of the missile or underwater running body. A signal proportional to the square of the speed of the missile or underwater running body from an external computer 2 is multiplied by the output of a steering angle detector 1 through a multiplier 6, whose output is fed to a gain adjustment device 7. Then, its output is passed through a torque amplifier 4 to operate a torquer 5, and consequently a load is applied to the steering wing on real-time basis without any influence upon intervals of the calculation of the external computer 2, thus improving the response performance of a simulator.
JP55167543A 1980-11-28 1980-11-28 Simulator of load on steering wing Pending JPS5791434A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55167543A JPS5791434A (en) 1980-11-28 1980-11-28 Simulator of load on steering wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55167543A JPS5791434A (en) 1980-11-28 1980-11-28 Simulator of load on steering wing

Publications (1)

Publication Number Publication Date
JPS5791434A true JPS5791434A (en) 1982-06-07

Family

ID=15851650

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55167543A Pending JPS5791434A (en) 1980-11-28 1980-11-28 Simulator of load on steering wing

Country Status (1)

Country Link
JP (1) JPS5791434A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102642624A (en) * 2012-05-11 2012-08-22 中国航空工业集团公司西安飞机设计研究所 Load simulator of plane booster dummy assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102642624A (en) * 2012-05-11 2012-08-22 中国航空工业集团公司西安飞机设计研究所 Load simulator of plane booster dummy assembly
CN102642624B (en) * 2012-05-11 2014-08-06 中国航空工业集团公司西安飞机设计研究所 Load simulator of plane booster dummy assembly

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