Analytic solution of the problem of stabilizing orbital orientation of a spacecraft with flywheel engines
Author:
Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0036155
Reference21 articles.
1. Space Station attitude control and momentum management - A nonlinearlook
2. Implementation of the Orbital Orientation Mode of an Artificial Satellite of the Earth without Accumulation of the Angular Momentum of the Gyro System
3. Studying the Possibility of Ensuring the Stabilization Accuracy Characteristics of an Advanced Spacecraft for Remote Sensing of the Earth
4. On an adaptive control system for angular motion of a communication satellite
5. Geometric Mechanics Based Nonlinear Model Predictive Spacecraft Attitude Control with Reaction Wheels
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