Article

Article title ALGORITHM OF HIERARCHICAL DE-COMPOSITION OF AIRCRAFT CONTROL DESIGN PROCEDURE
Authors A.S. Mushenko
Section SECTION III. ALGORITHMIC AND THE SOFTWARE
Month, Year 05, 2013 @en
Index UDC 681.5
DOI
Abstract In the paper we explore the hierarchical approach to aircraft spatial motion co-related control design basing on 12-th order nonlinear math. model of rigid body motion. We provide the algorithm of deriving the design procedure into three stage. The top level provides the base control laws. By using of known algebraic coupling equation describing dependence between united vector of forces and moments of forces, and aerodynamic coefficients and control surface deflection angles for special aircraft, we present the technique of control law design for middle-level control basing of universal united control laws of top-level. The middle-level laws may be used as a desired values for local automation systems for aircraft actuators control.

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Keywords Aircraft; ADAR method; synergetic control theory; nonlinear control; dynamics of flight; hierarchical control.
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