V. Agapov

ORCID: 0000-0002-0122-1628
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About
Contact & Profiles
Research Areas
  • Space Satellite Systems and Control
  • Astro and Planetary Science
  • Astronomical Observations and Instrumentation
  • Planetary Science and Exploration
  • GNSS positioning and interference
  • Space exploration and regulation
  • Geophysics and Gravity Measurements
  • Spacecraft Design and Technology
  • Advanced Research in Science and Engineering
  • Radio Astronomy Observations and Technology
  • Laser-induced spectroscopy and plasma
  • Astronomy and Astrophysical Research
  • Geochemistry and Geologic Mapping
  • High-Velocity Impact and Material Behavior
  • CCD and CMOS Imaging Sensors
  • Ionosphere and magnetosphere dynamics
  • Science, Technology, and Education in Latin America
  • earthquake and tectonic studies
  • Aerospace Engineering and Energy Systems
  • Field-Flow Fractionation Techniques
  • Image Processing and 3D Reconstruction
  • Statistical and numerical algorithms
  • Advanced Optical Sensing Technologies
  • Space Science and Extraterrestrial Life
  • Inertial Sensor and Navigation

Keldysh Institute of Applied Mathematics
2004-2022

Russian Academy of Natural Sciences
2007

Pulkovo Observatory
2004

10.1016/j.asr.2005.03.022 article EN Advances in Space Research 2005-01-01

Operations in geosynchronous orbit are important for many aspects of commerce. Avoiding conjunctions an ever increasingly crowded environment is therefore becoming more especially light the Iridium 33 / Cosmos 2251 collision. SOCRATES-GEO has combined owner operator numerical ephemerides with Two-Line Element (TLE) set information over 2 years. Unfortunately, TLE limited quality, and obtaining high quality often difficult. Previously we explored how could replace data those objects which do...

10.2514/6.2010-7525 article EN AIAA/AAS Astrodynamics Specialist Conference 2010-06-14

The method presented in this paper is developed to assess the parameters (the application moment and magnitude of a velocity impulse) maneuver-like perturbation motion center mass spacecraft near-circular orbit. assessment based on information spacecraft’s trajectory before maneuver optical observations angular position (right ascension declination angles) after maneuver. This study considers cases solely transversal (in-track) or radial components increment vector. A single pair values...

10.3390/sym14122564 article EN Symmetry 2022-12-05

10.2514/6.iac-06-b6.p.1.04 article EN 57th International Astronautical Congress 2006-10-02
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