Thermally Induced Attitude Dynamics of a Spacecraft with a Flexible Appendage
Guardado en:
| Autor principal: | Johnston, J. D. |
|---|---|
| Otros Autores: | Thornton, E. A. |
| Formato: | Artículo |
| Lenguaje: | Inglés |
| Aporte de: | Registro referencial: Solicitar el recurso aquí |
Ejemplares similares
-
Active Vibration Suppression in Flexible Spacecraft Attitude Tracking
por: Di Gennaro, S. -
Rapid Reorientation Maneuvers of Experimental Spacecraft with a Pendulum Appendage
por: Li, F. -
Fundamentals of Spacecraft Attitude Determination and Control
por: Markley, F. Landis
Publicado: (2014) -
Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertial Matrix Identification
por: Ahmed, J. -
Nonlinear Input Shaping Control of Flexible Spacecraft Reorientation Maneuver
por: Gorinevsky, D.