Solving of the some special control problems of launch vehicle at the initial flight part using the AKOR method-Reference-Cited by-同舟云学术

Solving of the some special control problems of launch vehicle at the initial flight part using the AKOR method

Published:2021 Issue: Volume: Page:
ISSN:0094-243X
Container-title:XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration
language:
Short-container-title:

Author:

Bobronnikov Vladimir,Trifonov Maksim

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0035720

Reference21 articles.

1. Lossless Convexification of Nonconvex Control Bound and Pointing Constraints of the Soft Landing Optimal Control Problem

2. Research the opportunities of passive aerodynamic stabilization of the launch vehicle fairing shells

3. A.S. Filatyev and A. Golikov, “New features of unguided body reentry with subcircular velocity and peculiarities of its simulation,” in 29th Congress of the International Council of the Aeronautical Sciences (ICAS), 2014.

4. Concept development of control system for perspective unmanned aerial vehicles

5. A.Sh. Altshuler, V.T. Bobronnikov and M.V. Trifonov, Development of launch vehicle control algorithm for the initial part of the trajectory using the ACOR method, Siberian Journal of Science and Technology 18(2), 314– 322 (2017).

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Distribution of Information Flows in Orbital Groupings for Remote Sensing of the Earth;Russian Engineering Research;2022-01

2. Formation of the orbital parameters of promising satellite for earth remote sensing;PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON ENGINEERING RESEARCH 2021 (ICER 2021), MOSCOW, RUSSIA;2022