The paper analyses the launching missiles stability of aircraft with auto-flight system, and simulates the process of launching and optimizes the control law of the auto-flight system.
文中对带有自动驾驶仪飞机投弹的稳定性进行了分析，对其过程进行了仿真研究和控制律优化设计。
The paper analyses the launching missiles stability of aircraft with auto-flight system, and simulates the process of launching and optimizes the control law of the auto-flight system.
文中对带有自动驾驶仪飞机投弹的稳定性进行了分析，对其过程进行了仿真研究和控制律优化设计。
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