Roll control of a flight vehicle with the adjustable center of mass


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

详细

We present the results of analytical research of flight dynamics for a flight vehicle that is controlled by the adjustable center of mass in the vertical symmetry plane. The roll oscillations, which appear perpendicular to the symmetry plane due to technological errors, are eliminated by means of control rocket engines, for which a control law is assigned.

作者简介

V. Afanas’ev

South Ural State University (National Research University)

编辑信件的主要联系方式.
Email: mas41@list.ru
俄罗斯联邦, pr. Oktyabrya 16, Miass, 456318

G. Degtyarev

Tupolev Kazan National Research Technical University

Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111

V. Kiselev

South Ural State University (National Research University)

Email: mas41@list.ru
俄罗斯联邦, pr. Oktyabrya 16, Miass, 456318

A. Meshchanov

Tupolev Kazan National Research Technical University

Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111

补充文件

附件文件
动作
1. JATS XML

版权所有 © Allerton Press, Inc., 2017