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
IEEE Aerospace and Electronic Systems Magazine ; 6 , 2 ; 3-7
1991-02-01
404646 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Monte Carlo Analysis of Titan-Transfer Orbit Stage Planetary Mission Guidance System
Online Contents | 1995
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