Satellite attitude dynamics and control in presence of environmentaltorques - A brief survey

Author:

SHRIVASTAVA S.1,MODI V.2

Affiliation:

1. Indian Institute of Science, Bangalore, India

2. British Columbia, University, Vancouver, Canada

Publisher

American Institute of Aeronautics and Astronautics

Reference286 articles.

1. authors 14, 4,30,31133,75-39 et The presence

2. aXis 40-44 e t al. For a more accurate model, the known magnetic field data a t various points in space can be combined together by s herical harmonic expansion using a digital computer 4'. A t high altitudes, the field gets a£fected by the sun-spot activity and solar emissions. Using this simple model, many authors have determined the ma torque acting on a satellite 4''30 "4"'it a1.

3. considerable attention 33' 45-4 '. In modelling the

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