The integrated flight control system test equipment constituted by the test software and hardware system.
该软件配合硬件系统，可组成飞控系统综合测试设备。
This paper proposes an approach of integrated analysis of performance and reliability for missile's flight control system under the effects of some important factors.
提出了在几种主要因素影响下进行飞控系统性能和可靠性一体化分析的方法。
In this paper, the authors try to apply neutral stability mode of the aircraft direct force Control technology to the air-to-air gunnery mode of the integrated flight/fire control system.
本文提出飞机中性稳定技术应用于综合火力 /飞行控制系统 ，给出了中性稳定飞机结构图和动力学模型。
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