Inertial Attitude Control System
Key Facts
Abbreviation
IACS
Pronunciation
/ˌɪˈnərʃəl ˈætəˌtud kənˈtroʊl ˈsɪstəm/
Category
Governmental
Related Field
NASA
Examples in Context
- The paper presents the working principles and condition characteristics of inertial sensor in attitude control system of satellite, and analyzes key techniques of satellite inertial sensor such as longevity, thermal-vacuum and anti-radiation, etc.
- Reaction wheel ( RW ) is one of the most important inertial execution parts of satellite attitude control system, it is widely used as the main execution part in three-axis stabilization satellite that with long life, high precision, multifunctional which be launched in recent few years.