Two algorithms were developed to demonstrate the implementation of autonomous functions in an existing spacecraft power system. The functions selected for autonomous operation include a typical performance monitoring function, battery state of charge, and a fault detection and response function represented by a battery state of charge below a preselected limit. The constraints imposed by the existing power system configuration are the available data in the telemetry stream and the existing commands and command structure. The areas requiring future development are the degree of battery characterization, the effects of hardware/software faults, and the verification of faults.
Algorithm development for a spacecraft autonomous power system
Entwicklung eines Algorithmus fuer ein autonomes Energiesystem in einem Raumschiff
1983
5 Seiten, 5 Bilder, 2 Tabellen, 5 Quellen
Conference paper
English
Spacecraft electrical power autonomous management system
IEEE | 2014
|Large Autonomous Spacecraft Electrical Power System (LASEPS)
SAE Technical Papers | 1992
|A Fast Autonomous Star Acquisition Algorithm for Spacecraft
British Library Conference Proceedings | 1997
|METHOD TO CONTROL AUTONOMOUS SYSTEM OF SPACECRAFT POWER SUPPLY
European Patent Office | 2016
|