Г. А. Иванова

ORCID: 0000-0002-7400-3648
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About
Contact & Profiles
Research Areas
  • Inertial Sensor and Navigation
  • Spacecraft Design and Technology
  • Geological Modeling and Analysis
  • Rocket and propulsion systems research
  • Aerospace Engineering and Control Systems
  • Geomagnetism and Paleomagnetism Studies
  • Geodetic Measurements and Engineering Structures
  • Polymer Science and Applications
  • Material Properties and Applications
  • Cybersecurity and Information Systems
  • Engineering Education and Technology
  • Electric Power Systems and Control
  • Heat Transfer and Mathematical Modeling
  • 3D Surveying and Cultural Heritage
  • Advanced Research in Systems and Signal Processing
  • Geophysical and Geoelectrical Methods
  • Geotechnical and Geomechanical Engineering
  • Spacecraft Dynamics and Control
  • Spacecraft and Cryogenic Technologies
  • Engineering Diagnostics and Reliability
  • Industrial Engineering and Technologies
  • Engineering Applied Research
  • Field-Flow Fractionation Techniques
  • Diverse Industrial Engineering Technologies
  • Magnetic Field Sensors Techniques

Ufa State Aviation Technical University
2014-2016

Yuzhnoye State Design Office (Ukraine)
2011

East Institute Refractories (Russia)
1991

Institute of Metallurgy
1989

The Electric Power Subsystem (EPS) is one of the most critical system on any satellite because nearly every other subsystem requires power.This makes choice power systems important task facing designers.The main purpose Satellite EPS to provide continuous, regulated and conditioned all subsystems.It has do that withstanding radiation, thermal cycling, vacuum a hostile space environment as well degradation over time [1].The characteristics are determined by both parameters itself orbit RI...

10.21608/asat.2011.27197 article EN International Conference on Aerospace Sciences and Aviation Technology 2011-05-01

The article dwells on the spacecraft attitude control to point onboard antenna ground data acquisition station during communication session. Antenna is fixed relative body. Pur-pose of receive flight task aboard and downlink telemetry infor-mation. When orbiting, position changes contin-uously. It due diurnal rotation Earth, orbital motion angular center mass under impact disturbing moments. To tilt uses reaction wheels, installed in axes coordinate system coupled with mass. Electromagnets...

10.33136/stma2023.01.041 article EN Kosmičeskaâ tehnika Raketnoe vooruženie 2023-05-12

This article covers material on features and prospects for the use of gyroscopic device in inclinometer. Furnishes way to carry out a choice angular-rate sensor measuring module deviation survey using Pareto integral criterions.

10.17122/ngdelo-2012-1-152-158 article EN Нефтегазовое дело 2012-03-01

10.33136/stma2019.01.015 article EN Kosmičeskaâ tehnika Raketnoe vooruženie 2019-02-12
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