A. Sedelnikov

发表

Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. II

A. Sedelnikov, 2007 .

Evaluation of the Level of Microaccelerations on-Board of a Small Satellite Caused by a Collision of a Space Debris Particle with a Solar Panel

A. Sedelnikov, 2016 .

Modeling the disturbing effect on the aist small spacecraft based on the measurements data

V. Salmin, A. Sedelnikov, 2022, Scientific Reports.

Construction of the Criterion for Using a Two-dimensional Thermal Conductivity Model to Describe the Stress–strain State of a Thin Plate Under the Thermal Shock

A. Sedelnikov, V. Serdakova, E. Khnyryova, 2021, Microgravity Science and Technology.

Analysis of the Significance of the Influence of Various Components of the Disturbance from a Temperature Shock on the Level of Microaccelerations in the Internal Environment of a Small Spacecraft

A. Sedelnikov, D. Orlov, 2021, Microgravity Science and Technology.

Investigation of the dynamics of a small spacecraft elastic element temperature change under a temperature shock considering a penumbral section

A. Sedelnikov, D. Orlov, Yu D Leskova, 2021 .

Development of Control Algorithms for the Orbital Motion of a Small Technological Spacecraft with a Shadow Portion of the Orbit

A. V. Sedelnikov, D. I. Orlov, A. Sedelnikov, 2020, Microgravity Science and Technology.

Accuracy assessment of microaccelerations simulation on the spacecraft “Foton-M” no. 2 according to magnetic measuring instruments data

A. V. Sedelnikov, A. Sedelnikov, 2020 .

Accuracy assessment of microaccelerations simulation on the spacecraft “Foton-M” no. 2 according to magnetic measuring instruments data

A. Sedelnikov, 2019, Microgravity Science and Technology.

The simulation results of the operation of a small spacecraft motion control system with an electrothermal microdrive

A. Sedelnikov, A. Belousov, A. S. Gorozhakina, 2019, Journal of Physics: Conference Series.

How Does Asymmetry of Solar Panels Influence Constructive Component of Microacceleration Field of Inner Environment of Space Laboratory

K. I. Potienko, A. Sedelnikov, D. P. Molyavko, 2017, Microgravity Science and Technology.

Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements

A. Sedelnikov, 2016, Microgravity, science and technology.

How to Estimate Microaccelerations for Spacecraft with Elliptical Orbit

K. I. Potienko, A. Sedelnikov, 2015, Microgravity Science and Technology.

CONTROL OF MICROACCELERATIONS AS THE MAJOR CHARACTERISTICS OF SPACE LABORATORY OF SPECIALIZED TECHNOLOGICAL APPOINTMENT AS CONSTRUCTIVE METHODS

A. V. Sedelnikov, A. Sedelnikov, 2014 .

Analysis of micro-acceleration requirements in the context of designing a small technological spacecraft

A I Belousov, A V Sedelnikov, G P Anshakov, 2021 .

Restoration of the current signal from solar panels of AIST small spacecraft for estimate the parameters of the rotational motion

A. Sedelnikov, T. A. Ivashova, S. Safronov, 2020, Journal of Physics: Conference Series.

Mean of Microaccelerations Estimate in the Small Spacecraft Internal Environment with the Use of Fuzzy Sets

A. Sedelnikov, 2018, Microgravity Science and Technology.

Investigation of the rotational motion stability of the aist small spacecraft prototype according to the measurements of the earth’s magnetic field

A. Sedelnikov, A. Taneeva, E. Khnyryova, 2021 .

Control of rotational motion of a partially inoperable small spacecraft using fuzzy sets

S L Safronov, A V Sedelnikov, E S Khnyreva, 2019, Journal of Physics: Conference Series.