Total Energy Control of Aircraft Longitudinal Motion

IF 0.5 Q4 PHYSICS, MULTIDISCIPLINARY

Optoelectronics Instrumentation and Data Processing Pub Date : 2024-03-08 DOI:10.3103/s8756699023050011

S. A. Belokon, Yu. N. Zolotukhin, K. Yu. Kotov, A. S. Maltsev, A. P. Yan

引用次数: 0

Abstract

The paper considers the creation of a system for controlling the longitudinal motion of aircraft based on the principle of total energy control. The structure of the control system is presented, including a kernel independent of aircraft and a transition to commands for elevator and thrust deflection obtained from the principle of inverse models. The control system is implemented for models of three aircraft with different aerodynamic configurations. The quality of regulation was studied by numerical simulation.

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飞机纵向运动的总能量控制

摘要本文探讨了根据总能量控制原理创建飞机纵向运动控制系统的问题。文中介绍了控制系统的结构，包括一个独立于飞机的内核，以及根据逆模型原理获得的升降舵和推力偏转指令的过渡。该控制系统针对具有不同气动配置的三种飞机模型实施。通过数值模拟对调节质量进行了研究。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

Optoelectronics Instrumentation and Data Processing PHYSICS, MULTIDISCIPLINARY-

CiteScore

1.00

自引率

50.00%

发文量

期刊介绍： The scope of Optoelectronics, Instrumentation and Data Processing encompasses, but is not restricted to, the following areas: analysis and synthesis of signals and images; artificial intelligence methods; automated measurement systems; physicotechnical foundations of micro- and optoelectronics; optical information technologies; systems and components; modelling in physicotechnical research; laser physics applications; computer networks and data transmission systems. The journal publishes original papers, reviews, and short communications in order to provide the widest possible coverage of latest research and development in its chosen field.