CAJ | 학술논문

　　舰载预警机复飞时，需要通过加大发动机推力提高飞行速度，从而增加其升力以使航迹下沉量减少，避免与舰尾相撞。在分析舰载预警机复飞准则的基础上，通过建立舰载预警机着舰复飞时的非线性动力学方程，计算分析了不同速度、不同下沉率时舰载预警机的复飞轨迹和复飞边界。仿真结果表明：适当的复飞决策距离和较大的发动机推力，可保证舰载预警机安全复飞。
　　함재예경궤복비시，수요통과가대발동궤추력제고비행속도，종이증가기승력이사항적하침량감소，피면여함미상당。재분석함재예경궤복비준칙적기출상，통과건립함재예경궤착함복비시적비선성동역학방정，계산분석료불동속도、불동하침솔시함재예경궤적복비궤적화복비변계。방진결과표명：괄당적복비결책거리화교대적발동궤추력，가보증함재예경궤안전복비。
When the carrier-based (Air Early Warning), AEW waves off,the engine thrust should be increased to achieve high velocity. And then the AEW has enough lift to avoid collision with the carrier. The wave off rules and decision system for wave off were established to improve the landing safety of the AEW. The wave off capability of the carrier-based AEW. Based on nonlinear flight dynamic model, the wave off track and bor?derline were analyzed according to the various velocity and sinking rate of the AEW was deal with. The results of the simulation in this paper showed that the proper wave off decision distance and the powerful engine thrust could ensure wave off safety of the carrier-based AEW.