Procedure of assessing precision parameters of satellite astro-inertial system with development of a model for estimating observabiliti of navigational-aid satellites.
Navigation systems
Аuthors
1*, 21. Air Force Central Research Institute of the Ministry of Defense of the Russian Federation, 2-5, Aerodromnaya str, Shchelkovo, Moscow region, 141103, Russia
2. ,
*e-mail: vin1985000@mail.ru
Abstract
A structural scheme of procedure for a priory assessment of location precision with the aid of satellite astro-inertial system as well as a model and relations for estimating observability of navigational-aid satellites are presented. Examples of observability determination are suggested.Keywords:
satellite astro-inertial system; precision assessment; observability.Download