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- Article name
- CONDITIONS FOR CREATING AN ARTIFICIAL GEOSTATIONARY ORBIT AND A MATHEMATICAL MODEL FOR DETERMINING ANGULAR ABERRATION DURING LASER LOCATION OF A SPACECRAFT IN THIS ORBIT
- Authors
- Zinacheva T. S., , zino4k@bk.ru, Moscow Aviation Institute (National Research University), Moscow, Russia
Denisov M. M., , dmm11@inbox.ru, Moscow Aviation Institute (National Research University), Moscow, Russia
- Keywords
- laser location / geostationary orbit / the angular aberration
- Year
- 2019 Issue 3 Pages 59 - 64
- Code EDN
- Code DOI
- Abstract
- An equation is derived from which the magnitude and direction vector of the engine thrust force will be determined, allowing the spacecraft to be held above or below the natural geostationary orbit. A mathematical model of a laser location of a spacecraft located on artificial geostationary orbits in a rotating reference frame has been built. A formula for calculating the angular aberration, which occurs when taking into account the non-inertial reference system, is derived. The maximum and minimum values of the angular aberration are calculated when the spacecraft is located in the created orbits.
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