建立了某型双发舰载机正常状态及单发停车故障状态动力学模型。采用牛顿迭代法,运用Matlab仿真环境完成了单发停车等角下滑着舰飞行过程的配平计算与分析。结果表明,某型舰载机单发停车时能够实现下滑着舰状态的飞行动力学平衡控制,可为单发停车故障时飞行员进行着舰操纵提供参考,为后续进行飞行控制系统故障重构控制律设计奠定基础。 The dynamic model of the normal state of a certain type of twin-engine ship-borne aircraft and the single-state parking fault status is established. Using Newton’s iteration method, using Matlab simulation environment to complete the single-stop parking taxiing process equi-level calculation and analysis. The results show that a certain type of carrier-based aircraft can achieve the flight dynamics balance control of the gliding state when it is stopped by a single carrier, which can provide a reference for the pilots to steer and maneuver in the event of single-vehicle parking failure. Law design laid the foundation.