The purpose of the Flight Experiment Demonstration System (FEDS) was to show, in a simulated spacecraft environment, the feasibility of using a microprocessor to automate the onboard orbit determination functions. The software and hardware configuration used to support FEDS during the demonstration and the results of the demonstration are discussed.
Flight Experiment Demonstration System (FEDS) Analysis Report
1986
323 pages
Report
No indication
English
Unmanned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Airborne/spaceborne computers , Orbital position estimation , Space environment simulation , Spacecraft control , Data transmission , Microprocessors , Spacecraft communication , Spacecraft orbits , Tdr satellites , Computer programs , Spacecraft environments , Transponders , FEDS system
Online Contents | 2009
Online Contents | 2009