Abstract The system of spacecraft angular stabilization of middle accuracy rating and with magnetic executive devices is considered. A three-axis magnetometer is used as a single sensitive element of the subsystem of attitude determination. Combination of specific features of the control law and the algorithm of attitude determination allows one to realize a sufficiently reliable stabilization system of simple design, which is rather economical, as far as computing time is concerned.
Magnetic stabilization of a spacecraft and the effect of compensation of information errors
Cosmic Research ; 50 , 1
2012
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung | |
Lokalklassifikation TIB: | 770/3520/8000 |
Magnetic stabilization of a spacecraft and the effect of compensation of information errors
Springer Verlag | 2012
|Magnetic spacecraft attitude stabilization with two torquers
Elsevier | 2021
|Spacecraft stabilization system
Online Contents | 1995
Errors Within the Time Transfer Model and Compensation Methods for Earth-Orbing Spacecraft
Springer Verlag | 2020
|