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Priority to UA20031213190ApriorityCriticalpatent/UA67704C2/en
Publication of UA67704ApublicationCriticalpatent/UA67704A/en
Publication of UA67704C2publicationCriticalpatent/UA67704C2/en
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.
UA20031213190A2003-12-302003-12-30Method for pitch and yaw control
UA67704C2
(en)
Control instructions elaborating method for autopilot or command elaborator, involves measuring parameter of yaw movement and introducing corrective term of coupling in evaluation of control instructions