Defining the Spacecraft Angular Position in the Orbital Stabilization Mode from the Angular Rate Sensor Measurements

Defining the Spacecraft Angular Position in the Orbital Stabilization Mode from the Angular Rate Sensor Measurements

<p>The spacecraft orientation mode relative to given reference point is implemented using the sensor equipment, which measures the spacecraft angular position relative to given reference coordinate system and the angular rate of the spacecraft rotation relative to inertial space. In case one o...

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Bibliographic Details
Main Authors: A. S. Oleynik, N. E. Zubov, V. N. Ryabchenko
Format: Article
Language:Russian
Published: MGTU im. N.È. Baumana 2015-01-01
Series:Nauka i Obrazovanie
Subjects:
spacecraft
exact placement of the poles method
state vector
angular velocity
estimation algorithm
Online Access:http://technomag.edu.ru/jour/article/view/180

Internet

http://technomag.edu.ru/jour/article/view/180

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