The ever increasing complexity of Earth observation spacecraft requires new verification methods and powerful test support equipments. An overall approach is presented for the spacecraft from electrical assembly and tests up to validation of flight operational procedures, together with guidelines for optimized design of the required check out and verification ground equipments. These test methods and verification steps were implemented on SPOT and ERS 1 programs.
Final Validation of Autonomous Spacecraft
1990
4 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Space Launch Vehicles & Support Equipment , Checkout , Earth observations (From space) , Flight simulators , Ground support equipment , Onboard data processing , Program verification (Computers) , Autonomy , Ers-1 (Esa satellite) , European space agency , Spot (French satellite) , Foreign technology
Tema Archiv | 1986
|NTRS | 1982
|Operations for Autonomous Spacecraft
IEEE | 2022
|