Kinematics Modeling for Satellite Antenna Dish Stabilized Platform

In this paper, the kinematics model of the satellite antenna dish three-axis platform is developed, and the detailed formulation of these equations for the stable member is presented. The x, z, y Euler sequence is used to represent the kinematics models. By using the principle of Level maintenance, it has been investigated the intrinsic properties including the Euler angle variation of the platform, the angular speed and the angular acceleration of each part of the system. These results provide practical guidelines for promoting the utilization and popularization of the ship carried stabilized platform. By using a matlab simulation we show the angular velocities variation of the ship platform. Simulation results are also represented in this paper.