SYSTEM OF SPACECRAFT GEOPHYSICAL SAFETY Russian patent published in 2014 - IPC B64G3/00 

FIELD: aircraft engineering.

SUBSTANCE: geophysical safety system for spacecraft (SC) consists of geophysical data acquisition module 1 and SC flight parameters data base unit 2 with their outputs connected to processing and analysis module (PAM) 4. Data from SC onboard hardware performances data base 3 to PAM input to compare the data on SC medium and path is fed to PAM input. PAM output is connected to medium influence allowance guidelines issue module (MIAGIM) 6 generating SC control guidelines proceeding from obtained data and possible safety measures from data base of standard scripts 5. MIAGIM signals are fed to spacecraft onboard hardware application permit module (APM) 7 and to operating command tab module (OCTM) 11. APM output is connected with onboard hardware operation scheduling module (OSM) 12. APM operation is based on flight program data base 8 connected therewith to define hardware possible jobs without detriment to spacecraft target tasks and on data base of the ground automated control complex schedule of operation. Data of spacecraft onboard hardware state control module 9 is fed to APM input. OCTM output is connected with spacecraft flight program control module 13 that tracks actual execution of loaded instructions.

EFFECT: longer life of onboard hardware.

1 dwg