[PDF][PDF] Improving the spacecraft center of mass stabilization accuracy
N Zosimovych - IOSR Journ. of Eng.(IOSRJEN), 2017 - researchgate.net
The publication suggests how to significantly improve the spacecraft center of mass
movement stabilization accuracy in the active phases of trajectory correction during …
movement stabilization accuracy in the active phases of trajectory correction during …
[PDF][PDF] Invariant Stabilization Algorithms in a Control System with Rotating Operating Device
N Zosimovych - American Journ. of Eng. Research (AJER), 2017 - researchgate.net
The publication suggests how to significantly improve the spacecraft center of mass
movement stabilization accuracy in the active phases of trajectory correction during …
movement stabilization accuracy in the active phases of trajectory correction during …
Sounding rocket preliminary design
N Zosimovych - European Journal of Engineering and Technology …, 2021 - ej-eng.org
This article aims at studying sounding rocket (SR) class, or those vehicles launched from the
earth and carrying out various experiments at high altitudes. After the end of their mission …
earth and carrying out various experiments at high altitudes. After the end of their mission …
[PDF][PDF] Modeling of Transition Processes in a Partially Invariant Center of Mass Motion Stabilization System
N Zosimovych - Int. Journ. of Aerospace Sc, 2017 - academia.edu
The publication suggests how to significantly improve the spacecraft centre of mass
movement stabilization accuracy in the active phases of trajectory correction during …
movement stabilization accuracy in the active phases of trajectory correction during …
[PDF][PDF] Smallsat Rational Design
N Zosimovych, X Niu, A Simeone, X Peng - J Appl Mech Eng, 2018 - researchgate.net
This paper is devoted to the study of CubeSat rational designing technique. The CubeSat
design process is comprised of choice of its trajectory, determination of components and …
design process is comprised of choice of its trajectory, determination of components and …
Spacecraft's Partially Invariant Stabilization System
N Zosimovych - IOP Conference Series: Materials Science and …, 2020 - iopscience.iop.org
In most of the known spacecraft stabilization systems the control signal in the centre of mass
movement channel is generated according to proportional plus integral control law, based …
movement channel is generated according to proportional plus integral control law, based …
[PDF][PDF] Partially Invariant System for Spacecraft Center of Mass Motion Stabilization
N Zosimovych - 2019 - researchgate.net
This publication suggests how we can improve the spacecraft centre of mass movement
stabilization accuracy in the active phases of trajectory correction. It will be during …
stabilization accuracy in the active phases of trajectory correction. It will be during …
[PDF][PDF] SmallSats Rational Design Technique
N Zosimovych - researchgate.net
The SmallSat design process is comprised of choice of its trajectory, determination of its
components and main parameters of its systems, development of external and internal …
components and main parameters of its systems, development of external and internal …
Stability Area of a Spacecraft's Partially Invariant Centre of Mass Motion Stabilization System
N Zosimovych - IOP Conference Series: Materials Science and …, 2019 - iopscience.iop.org
In practice, a spacecraft's stabilization system, which is partially invariant to the disturbing
moment, is the easiest to implement. The velocity performance limitation of the control …
moment, is the easiest to implement. The velocity performance limitation of the control …