The problems presented by the launch of a booster vehicle with a strapdown system on an expandable launch vehicle are addressed. These include the Earth motion by the wind-induced twist and sway motion at the launch pad, vibration-induced motion, and various sensor errors, as well as the limited memory and processing power of the flight computer. A robust numeric gyrocompass alignment algorithm is presented, and its performance in this environment is examined.
Transfer orbit stage gyrocompass alignment algorithm twist and sway environment for Mar's Observer mission on commercial Titan
Gyrokompaß-Regelalgorithmus für die Mars-Beobachtungsstation mit Titan-Rakete
IEEE Aerospace and Electronics Systems Magazine ; 6 , 2 ; 3-7
1991
5 Seiten, 4 Quellen
Aufsatz (Zeitschrift)
Englisch