| 2. | Secondly , at the premise of the basic hypothesizes , establish the “ astronaut - spaceship ” system dynamics equations based on the principle of momentum conservation , and simulate the disturbance influence of the spaceship attitude induced by five kinds astronaut ’ s motion include stand - up act , landing act , right arm single - pendulum motion , left arm double - pendulum motion , right arm operating panel motion
其次,在基本假设的前提下,基于动量矩守恒原理建立了“航天员?飞船”系统动力学方程,并仿真分析了起立动作、停靠动作、右臂单摆运动、左臂双摆运动和右臂操作仪表板五类航天员运动对飞船的姿态的扰动影响。 |
