本文介绍一个飞行调节系统,这一系统可使导弹在海面上空低空飞行。对调节器的构成、最优化的原则以及与特定导弹的匹配作了概述后,作为系统发展例子,介绍了通过部件到整个系统的实物模拟和飞行试验验证,逐步地对调节器-导弹系统进行试验的情况。 This article describes a flight control system that allows missiles to fly low over the sea. After summarizing the structure of regulator, the principle of optimization and matching with specific missiles, as an example of system development, the simulation and flight test verification of components through the whole system are introduced, and the regulator-missile system Test situation.