Problems in formation and control of a required microacceleration level at spacecraft design, tests, and operation von Belousov, A. I., Sedel’nikov, A. V.

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Modeling the disturbing effect on the aist small spacecraft based on the measurements data von Sedelnikov, A. V., Salmin, V. V.

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Estimating the Inertia Tensor Components of an Asymmetrical Spacecraft When Removing It from the Operational Orbit at the End of Its Active Life von Sedelnikov, A V, Orlov, D I, Bratkova, M E, Khnyryova, E S

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Probabilistic estimation of fulfilling favorable conditions to realize the gravity-sensitive processes aboard a space laboratory von Belousov, A. I., Sedel’nikov, A. V.

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Fractal assessment of microaccelerations at weak damping of natural oscillation in spacecraft elastic elements. II von Sedel'nikov, A V

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Simulation of a flexible spacecraft motion to evaluate microaccelerations von Sedel’nikov, A. V., Serpukhova, A. A.

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A problem of choosing a generalized parameter of flexible spacecraft structures to construct a fractal model of microaccelerations von Sedel’nikov, A. V.

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Investigation of the Stress-Strain State of a Rectangular Plate after a Temperature Shock von Sedelnikov, A. V., Orlov, D. I., Serdakova, V. V., Nikolaeva, A. S.

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Mean of Microaccelerations Estimate in the Small Spacecraft Internal Environment with the Use of Fuzzy Sets von Sedelnikov, A. V.

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

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The Assessment Problem of Microaccelerations at the Experimental Sample of the Small Spacecraft “AIST” after the Battery Degradation and the Method of its Solution von Sedelnikov, A. V.

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Development of Control Algorithms for the Orbital Motion of a Small Technological Spacecraft with a Shadow Portion of the Orbit von Sedelnikov, A. V., Orlov, D. I.

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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... von Sedelnikov, A. V., Orlov, D. I.

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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 von Sedelnikov, A.V., Serdakova, V. V., Khnyryova, E. S.

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Modeling of Microaccelerations Caused by Running of Attitude-Control Engines of Spacecraft with Elastic Structural Elements von Sedelnikov, A. V.

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Modeling the micro-acceleration field in the protected zone of vibration-proof devices for implementation of gravity-sensitive processes on board a small technological spacecraft von Sedelnikov, A. V., Taneeva, A. S.

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Classification of Microaccelerations According to Methods of their Control von Sedelnikov, A. V.

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Modeling the effect of temperature deformations of large elements on the dynamics of the orbital motion of a small spacecraft von Sedelnikov, A V, Rodina, V S, Orlov, D I

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Evaluation of calibration accuracy of magnetometer sensors of Aist small spacecraft von Sedelnikov, A V, Filippov, A S, Gorozhakina, A S

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Analysis of micro-acceleration requirements in the context of designing a small technological spacecraft von Anshakov, G P, Belousov, A I, Sedelnikov, A V, Taneeva, A S

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