UA67704A - Method for control by pitch and yaw - Google Patents

Method for control by pitch and yaw

Info

Publication number
UA67704A
UA67704A UA20031213190A UA20031213190A UA67704A UA 67704 A UA67704 A UA 67704A UA 20031213190 A UA20031213190 A UA 20031213190A UA 20031213190 A UA20031213190 A UA 20031213190A UA 67704 A UA67704 A UA 67704A
Authority
UA
Ukraine
Prior art keywords
control
rotation
pitch
yaw
disagreement
Prior art date
Application number
UA20031213190A
Other versions
UA67704C2 (en
Inventor
Borys Ivanovych Dotsenko
Vitalii Illich Korobov
Oleh Petrovych Korosteliov
Yevhen Viktorovych Kosovenko
Viacheslav Pavlovych Kuzmin
Oleksandr Fedorovych Nemchyn
Leonid Antonovych Semenov
Petro Oleksiiovych Yakovenko
Vitalii Vasyliovych Yakovliev
Original Assignee
Ltd Liability Company Company
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 Ltd Liability Company Company filed Critical Ltd Liability Company Company
Priority to UA20031213190A priority Critical patent/UA67704C2/en
Publication of UA67704A publication Critical patent/UA67704A/en
Publication of UA67704C2 publication Critical patent/UA67704C2/en

Links

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

A Method for controlling an aircraft (A) by pitch and yaw includes rotation of the A with respect to the longitudinal axis, formation of a control signal proportional to the deflection of the A from the support trajectory, its agreeing to the kinematical parameters of rotation of the A; that for one uses information on the angular velocity of rotation and the current value of the heel angle, this comes from the sensor of linear transversal overloading; control is processed by means of reversing steer drives in such a way that the control signals proportional to the coordinates of disagreement tend to zero.
UA20031213190A 2003-12-30 2003-12-30 Method for pitch and yaw control UA67704C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UA20031213190A UA67704C2 (en) 2003-12-30 2003-12-30 Method for pitch and yaw control

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UA20031213190A UA67704C2 (en) 2003-12-30 2003-12-30 Method for pitch and yaw control

Publications (2)

Publication Number Publication Date
UA67704A true UA67704A (en) 2004-06-15
UA67704C2 UA67704C2 (en) 2008-04-25

Family

ID=34513808

Family Applications (1)

Application Number Title Priority Date Filing Date
UA20031213190A UA67704C2 (en) 2003-12-30 2003-12-30 Method for pitch and yaw control

Country Status (1)

Country Link
UA (1) UA67704C2 (en)

Also Published As

Publication number Publication date
UA67704C2 (en) 2008-04-25

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