液体推进剂火箭运载器质量中心运动和推进剂消耗的终端控制

IF 0.6 4区计算机科学 Q4 AUTOMATION & CONTROL SYSTEMS Automation and Remote Control Pub Date : 2024-02-25 DOI:10.1134/s0005117923100041

V. P. Ivanov, V. K. Zavadskiy, A. A. Muranov, A. I. Chadaev, E. B. Kablova, L. G. Klenovaya, I. E. Tropova

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引用次数: 0

摘要

摘要我们将这部作品献给B.N. 彼得罗夫院士。它发展了他制定的火箭运载器终端控制原理。下一代火箭运载火箭采用质心运动和推进剂消耗相互联系、协调的末端控制原理。在这篇文章中，我们考虑了这种控制的综合问题及其实施的主要原则。

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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Terminal Control of Center of Mass Motion and Propellant Consumption in Liquid-Propellant Rocket Carriers

Abstract

We dedicate this work to the memory of Academician B.N. Petrov. It develops the principles of terminal control of rocket carriers formulated by him. Next-generation rocket carriers implement the principle of interconnected, coordinated terminal control of the center of mass motion and propellant consumption. In this article we consider the problem of synthesizing such control and the main principles of its implementation.

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来源期刊

Automation and Remote Control 工程技术-仪器仪表

CiteScore

1.70

自引率

28.60%

发文量

审稿时长

3-8 weeks

期刊介绍： Automation and Remote Control is one of the first journals on control theory. The scope of the journal is control theory problems and applications. The journal publishes reviews, original articles, and short communications (deterministic, stochastic, adaptive, and robust formulations) and its applications (computer control, components and instruments, process control, social and economy control, etc.).

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