For an A/A missile, its dynamics is separated into two parts, the dynamics of fast state and the dynamics of slow state based on the two timescale separation.

以某型空空导弹为对象，基于双时标的假设，将导弹动力学模态分离为快变状态动力学模态和慢变状态动力学模态，并对其分别进行了动态逆设计。

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And based on the time-scale separation principle, divided the control system into fast loop and slow loop, finish the six degrees of freedom nonlinear coordination simulation.

根据时标分离的原则，设计飞行器的快回路和慢回路控制器，并进行全包线六自由度非线性仿真。

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