JPS53124898A - Apparatus for controlling angle of flight attitude of airplane - Google Patents

Apparatus for controlling angle of flight attitude of airplane

Info

Publication number
JPS53124898A
JPS53124898A JP3888277A JP3888277A JPS53124898A JP S53124898 A JPS53124898 A JP S53124898A JP 3888277 A JP3888277 A JP 3888277A JP 3888277 A JP3888277 A JP 3888277A JP S53124898 A JPS53124898 A JP S53124898A
Authority
JP
Japan
Prior art keywords
airplane
flight attitude
angle
controlling angle
transmitting
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
JP3888277A
Other languages
Japanese (ja)
Other versions
JPS5853640B2 (en
Inventor
Ryoji Katayanagi
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP52038882A priority Critical patent/JPS5853640B2/en
Publication of JPS53124898A publication Critical patent/JPS53124898A/en
Publication of JPS5853640B2 publication Critical patent/JPS5853640B2/en
Expired legal-status Critical Current

Links

Abstract

PURPOSE: To provide an apparatus for controlling angle of flight attitude of airplane, which is capable of keeping flight path of the airplane in a fixed direction, by transmitting a part of flap actuating input force to elevators through a transfer function in changing angle of flight attitude, whereas transmitting a part of vertical-canard actuating input force to the rudder in changing the azimuth angle.
COPYRIGHT: (C)1978,JPO&Japio
JP52038882A 1977-04-05 1977-04-05 Aircraft attitude angle control device Expired JPS5853640B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP52038882A JPS5853640B2 (en) 1977-04-05 1977-04-05 Aircraft attitude angle control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP52038882A JPS5853640B2 (en) 1977-04-05 1977-04-05 Aircraft attitude angle control device

Publications (2)

Publication Number Publication Date
JPS53124898A true JPS53124898A (en) 1978-10-31
JPS5853640B2 JPS5853640B2 (en) 1983-11-30

Family

ID=12537572

Family Applications (1)

Application Number Title Priority Date Filing Date
JP52038882A Expired JPS5853640B2 (en) 1977-04-05 1977-04-05 Aircraft attitude angle control device

Country Status (1)

Country Link
JP (1) JPS5853640B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008543673A (en) * 2005-06-21 2008-12-04 ザ・ボーイング・カンパニー Aerospace aircraft yaw generation system and related methods

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60141245U (en) * 1984-02-29 1985-09-19 京セラ株式会社 thermal printing equipment

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS529445A (en) * 1975-07-11 1977-01-25 Nippon Telegr & Teleph Corp <Ntt> Fiber for long distance transmission
JPS5211109A (en) * 1975-07-17 1977-01-27 Ishikawajima Harima Heavy Ind Co Ltd Continuous raw material feed apparatus in vacuum melting furnaces

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS529445A (en) * 1975-07-11 1977-01-25 Nippon Telegr & Teleph Corp <Ntt> Fiber for long distance transmission
JPS5211109A (en) * 1975-07-17 1977-01-27 Ishikawajima Harima Heavy Ind Co Ltd Continuous raw material feed apparatus in vacuum melting furnaces

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008543673A (en) * 2005-06-21 2008-12-04 ザ・ボーイング・カンパニー Aerospace aircraft yaw generation system and related methods

Also Published As

Publication number Publication date
JPS5853640B2 (en) 1983-11-30

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