NASA NTRS · 19840024335
Flight Experiment Demonstration System (FEDS): Mathematical specification
Abstract
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.
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Shank, D. E.. 1984-07-01. Flight Experiment Demonstration System (FEDS): Mathematical specification. https://ntrs.nasa.gov/citations/19840024335
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