Modeling and Flight Data Analysis of Spacecraft Dynamics with a Large Solar Array Paddle

摘要

The Advanced Land Observing Satellite (ALOS) was launched on January 24, 2006 and has been operated successfully since then. This satellite has the attitude dynamics characterized by three large flexible structures, four large moving components, and stringent attitude/pointing stability requirements. In particular, it has one of the largest solar array paddles. Presented in this paper are flight data analyses and modeling of spacecraft attitude motion induced by the large solar array paddle. On-orbit attitude dynamics was first characterized and summarized. Three characteristic motions associated with the solar array paddle were identified and assessed. These motions are the thermally induced motion, the pitch excitation by the paddle drive, and the roll excitation. The thermally induced motion and the pitch excitation by the paddle drive were modeled and simulated to verify the mechanics of the motions. The control law updates implemented to mitigate the attitude vibrations are also reported.