Fail-safe gyromoment attitude control systems of communication, navigation, and land-survey satellites

Abstract

The bus development is based on broad NPO PM experience in designing and developing satellite systems. The bus was developed and tested to the extend as in the case of MSS-2500-GSO-01, but there's a need for conducting additional tests.The bus could be completely ready for integration in 18 month from the start of money investments.The bus in currently under development and its creation is based on the hardware shared from the MSS-2500-GSO-01 bus. The bus could be completely ready for integration in 24 month from the start of money investments.The bus price and the satellite price including the costs of its operation in orbit are brought under discussion when the exact project is at t h e development stage.Abstract: We present the new results about creation of fault-tolerant gyromoment attitude control systems (ACSs) for multipurpose and specialized spacecrafts (SCs) for communication, navigation and land-survey, application of matematical methods, and algorithms, and software for their dynamics investigations. 6