A procedure of optimal discrete synthesis for aircraft complexes basing on their formalized morphological analysis

Аuthors

Stepanov V. D.

4th Central Research Institute of the Russian Defense Ministry, 29, M.K. Tikhonravov str., Yubileyny , 141091, Russia

e-mail: svd1964@rambler.ru

Abstract

Optimal synthesis problems are considered for aircraft complexes assembled from units belong to a finite set of alternative subsystems. A statement and solution technique are suggested for the synthesis problem basing on optimal decomposition of the aircraft complex into groups of closely linked subsystems. Main principles are suggested to analyze morphologically the aircraft complex. Simulation results are presented as applies to a foundation of conventionally optimal updating ways for hypothetical aircraft complex of tactical aviation.

Keywords:

aircraft complex, synthesis, subsystem, combat effectiveness, cost, development time, optimization