This paper analyzed the different mechanism of interference and its effect in Missile-borne computer, and studies solution anti-interference design under two aspects of different mechanism.
分析了干扰在弹上计算机系统中的不同作用机理和影响，研究了两种不同作用效果下的抗干扰设计的解决办法。
But now the parameters of digital autopilot system can be easily designed, changed and loaded at real-time, at different flying states and at different Mach Numbers by missile-borne computer.
随着数字式弹载计算机的使用，自动驾驶仪能够很方便地实现系统变参数设计，在不同的马赫数及不同的飞行状态下，通过弹载计算机的解算来实时装订系统参数。
In order to realize high speed data communication between missile-borne computer and inertial navigation system, the engineering circuitry of data communication is designed.
为了实现弹载计算机和惯导的高速数据通信，对数据通信的工程化电路进行了设计。
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