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


Дәйексөз келтіру

Толық мәтін

Ашық рұқсат Ашық рұқсат
Рұқсат жабық Рұқсат берілді
Рұқсат жабық Тек жазылушылар үшін

Аннотация

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.

Авторлар туралы

V. Afanas’ev

South Ural State University (National Research University)

Хат алмасуға жауапты Автор.
Email: mas41@list.ru
Ресей, pr. Oktyabrya 16, Miass, 456318

G. Degtyarev

Tupolev Kazan National Research Technical University

Email: mas41@list.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111

V. Kiselev

South Ural State University (National Research University)

Email: mas41@list.ru
Ресей, pr. Oktyabrya 16, Miass, 456318

A. Meshchanov

Tupolev Kazan National Research Technical University

Email: mas41@list.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111

Қосымша файлдар

Қосымша файлдар
Әрекет
1. JATS XML

© Allerton Press, Inc., 2017