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本文提供了建立挠性卫星动力学模型的一种新方法。它和常规方法的比较表明,这两种方法得到的模型是一致的,但新方法更便于应用。文中还给出了应用新方法的一个典型例子。
This article provides a new approach to establishing a flexible satellite dynamics model. The comparison with the conventional method shows that the models obtained by the two methods are consistent, but the new method is more convenient to apply. The article also gives a typical example of the application of the new method.