ISO 20205:2015 pdf download.Space data and information transfer systems -Spacecraft Onboard lnterface Systems -Low Data-Rate Wireless Communications for Spacecraft Monitoring and Control.
2 OVERVIEVV
2.1 RATlOALE BENEFITS
Monitoring and controlling the behavior of a spacecraft and launch systems, during testing phases on ground or during nominal operations in orbit, is the key to ensuring the correct functioning of various onboard systems and structures, the responses of these systems in their operational working environments, and the long-ierm reliability of the spacecraft. These data are also highly significant when compiling lessons lcamcd that will be applied to building better space systems and increasing the reliability of future space components. (Refer to rcfcrcncc [3] for a comprehensive overview of application domains and for a dctailed summary of RF communications and restrictions in the thring operational environments)
The quantity of acquired spacecraft functional data depends on the ability to monitor required parameters at precise locations within a given project time and cost envelope. Hundreds and often thousands of data measurement locations are required, steadily increasing the mass (acquisition systems, cables, and harnesses) and the project costs and time (installation and verification of each new sensor).
2.1 RATlOALE BENEFITS
Monitoring and controlling the behavior of a spacecraft and launch systems, during testing phases on ground or during nominal operations in orbit, is the key to ensuring the correct functioning of various onboard systems and structures, the responses of these systems in their operational working environments, and the long-ierm reliability of the spacecraft. These data are also highly significant when compiling lessons lcamcd that will be applied to building better space systems and increasing the reliability of future space components. (Refer to rcfcrcncc [3] for a comprehensive overview of application domains and for a dctailed summary of RF communications and restrictions in the thring operational environments)
The quantity of acquired spacecraft functional data depends on the ability to monitor required parameters at precise locations within a given project time and cost envelope. Hundreds and often thousands of data measurement locations are required, steadily increasing the mass (acquisition systems, cables, and harnesses) and the project costs and time (installation and verification of each new sensor).
