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Abstract <p>Optimization of an aircraft vertical trajectory is considered. The central idea of this study is that a complex nonlinear boundary value problem is solved using a finite number of arithmetic operations. The results of numerical simulations confirm the efficiency of this technique.</p>

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On the Problem of Flight Dynamics

  • 期刊论文

  • 发表日期：

    2025年12月1日

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  • Yu. Ya. Ostov,
  • A. P. Ivanov

摘要

Abstract

Optimization of an aircraft vertical trajectory is considered. The central idea of this study is that a complex nonlinear boundary value problem is solved using a finite number of arithmetic operations. The results of numerical simulations confirm the efficiency of this technique.