Deployment Dynamics of Rotating Space Net

The deployment process of the rotating space net system is divided into two phases of arm deployment and net deployment. The system dynamic model is established according to different characteristics of the two phases. And the MK (Melnikov–Koshelev) control law is adopted. From the simulation of the rotating space net deployment process under MK control law, the anti-interference performance of stability and flight characteristics of the rotating space net, the effects of the centrifugal force and the damping are investigated.