To some flexible spacecraft with a rigid center hub and two identical flexible plates,it can't be simulated accurately depending on the model in[2]because the plate's length causes big elastic displacement. So this paper presents a method with which the system simulating model is built by partitioning the flexible plate into several parts and introducing the floating coordinate respectively. The control rule is designed by taking the plate as a whole. And numerical simulation is done .The simulating results show that this method is very efficient for big displacement.
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黄新生,陈荣娟.建立一类挠性航天器的动力学模型及面向控制的仿真环境. Building the Dynamics Model and Simulating Circumstances for theControl of a Kind of Flexible Spacecraft[J].国防科技大学学报,2003,25(1):84-87.