Simulation of the Longitudinal Carrier Landing in Different Sea-states for Carrier-based Aircraft

被引：0
|
作者：
Chen, Zhigang [1 ]
Han, Wei [1 ]
Chen, Junfeng [1 ]
Su, Xichao [1 ]
Ma, Xu [2 ]
机构：
[1] NAEU, Dept 1, Yantai, Shandong, Peoples R China
[2] PLA, 91467 Troops, Beijing, Peoples R China
来源：
2015 8TH INTERNATIONAL SYMPOSIUM ON COMPUTATIONAL INTELLIGENCE AND DESIGN (ISCID), VOL 1 | 2015年
关键词：
automatic carrier landing; sea-states; carrier motion; horizontal deviation;
D O I：
10.1109/ISCID.2015.257
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
The motion of aircraft carrier has much influence on the safety of the carrier-based aircraft landing process. The model of the carrier motion was established using harmonic equations. The pitch and heave of the carrier were calculated, as well as the movement of the desired touch-down point. The longitudinal landing motion model of aircraft was established with the small-disturbance equations. The automatic carrier landing of the F-18 aircraft at different sea-states was simulated. Considering the randomicity of the carrier motion, the random phase was introduced into the carrier motion equations. The model was simulated 200 times separately at sea-state 3, 4 and 5. The results show that the higher sea-states induces the severer carrier motion, thus the horizontal deviation of touch-down points gets larger and the success rate becomes lower.
引用
收藏
页码：474 / 477
页数：4
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