This paper analyzed the different mechanism of interference and its effect in Missile-bornecomputer, 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。
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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-bornecomputer.
In order to realize high speed data communication between missile-bornecomputer and inertial navigation system, the engineering circuitry of data communication is designed.