Control of flight vehicles with the adjustable center of mass


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详细

We resolve a problem how to control the longitudinal angular motion of flight vehicles (FV) having a system to displace the center of mass in the transverse direction. A structure is determined and a control law is established to start up and shutdown the engines. Formulas to determine the control parameters are obtained.

作者简介

V. Afanas’ev

South Ural State University

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

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

A. Meshchanov

Tupolev Kazan National Research Technical University

编辑信件的主要联系方式.
Email: mas41@list.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111

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