Computational models for the flight experiment demonstration system (FEDS) code 580 were developed. The FEDS is a modification of the automated orbit determination system which was developed during 1981 and 1982. The purpose of FEDS is to demonstrate, in a simulated spacecraft environment, the feasibility of using microprocessors to perform onboard orbit determination with limited ground support.
Flight Experiment Demonstration System (FEDS): Mathematical specification
01.07.1984
Report
Keine Angabe
Englisch
Online Contents | 2009
Online Contents | 2009