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现代飞机设计变化 ,增大了喷气战斗机出现惯性交感的可能性 ,致使某些飞机在高滚转速率下完全失稳。这种现象的数学分析通常是相当困难的。为此 ,本文利用简化线性分析法研究了惯性交感的影响因素和灵敏度 ,并借助计算机仿真手段确定了影响系统稳定性的参数和提供了通过附加航向及俯仰速率反馈进行人工稳定飞机的惯性交感控制系统
Changes in the design of modern aircraft have increased the likelihood of inertia sympathetic to jet fighters, causing some aircraft to be completely destabilized at high roll rates. Mathematical analysis of this phenomenon is often quite difficult. Therefore, in this paper, the simplified linear analysis method is used to study the influencing factors and sensitivities of inertial interaction, and the parameters that affect the stability of the system are determined by means of computer simulation. The inertial interaction control of artificial stabilized aircraft with additional heading and pitch rate feedback system