Attitude Control Synthesis for Small Satellites Using Gradient Method. Part I - Nonlinear Equations
The paper presents some aspects for synthesis of small satellites attitude control. Thesatellite nonlinear model presented here will be with six degrees of freedom. After movement equationlinearization the stability and command matrixes will be established and the controller will beobtained using gr...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2012-12-01
|
| Series: | INCAS Bulletin |
| Online Access: | http://nonlinear mode; small satellites; gradient methods; mathematical model |