JPS63108898U - - Google Patents

Info

Publication number
JPS63108898U
JPS63108898U JP26187U JP26187U JPS63108898U JP S63108898 U JPS63108898 U JP S63108898U JP 26187 U JP26187 U JP 26187U JP 26187 U JP26187 U JP 26187U JP S63108898 U JPS63108898 U JP S63108898U
Authority
JP
Japan
Prior art keywords
flap
output
speed detector
aircraft
computer
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
JP26187U
Other languages
English (en)
Japanese (ja)
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 filed Critical
Priority to JP26187U priority Critical patent/JPS63108898U/ja
Publication of JPS63108898U publication Critical patent/JPS63108898U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
JP26187U 1987-01-07 1987-01-07 Pending JPS63108898U (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP26187U JPS63108898U (zh) 1987-01-07 1987-01-07

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP26187U JPS63108898U (zh) 1987-01-07 1987-01-07

Publications (1)

Publication Number Publication Date
JPS63108898U true JPS63108898U (zh) 1988-07-13

Family

ID=30777070

Family Applications (1)

Application Number Title Priority Date Filing Date
JP26187U Pending JPS63108898U (zh) 1987-01-07 1987-01-07

Country Status (1)

Country Link
JP (1) JPS63108898U (zh)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009538779A (ja) * 2006-05-29 2009-11-12 エアバス フランス 高揚力形態において補助翼の制御を最適化する航空機の操縦方法および装置
JP2009539693A (ja) * 2006-06-13 2009-11-19 エアバス フランス 進入段階での航空機の操縦方法

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009538779A (ja) * 2006-05-29 2009-11-12 エアバス フランス 高揚力形態において補助翼の制御を最適化する航空機の操縦方法および装置
JP2009539693A (ja) * 2006-06-13 2009-11-19 エアバス フランス 進入段階での航空機の操縦方法

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