Errors of analog of inertial coordinate systems modeled in astronavigation system
Abstract
The errors of the simulation of an inertial coordinate system (ICS) in an astronavigation-system computer are derived as a function of errors of direction finding and the recording of the equatorial coordinates of the observed celestial bodies. It is shown that the derived relationships can be used in the analysis and synthesis of astronavigation systems as well as complex navigation systems.
- Publication:
-
USSR Rept Electron Elec Eng JPRS UEE
- Pub Date:
- December 1984
- Bibcode:
- 1984RpEEE....R...5K
- Keywords:
-
- Astronavigation;
- Error Analysis;
- Inertial Navigation;
- Space Navigation;
- Analogs;
- Celestial Navigation;
- Direction Finding;
- Inertial Coordinates;
- Vector Analysis;
- Space Communications, Spacecraft Communications, Command and Tracking