摘要
以歼击轰炸机为背景,根据实战要求假设作战环境和任务目标,对其在低空突防阶段的飞行轨迹、航时、油耗以及威胁概率等相关参数进行了研究分析,以期充分发挥飞机的潜在能力,提高作战效能,为实战使用和改进设计提供参考。对优化轨迹的仿真研究表明,所得出的战术飞行轨迹优化设计结果是合理的,同时也证实了战术飞行轨迹优化设计的有效性和可行性。
Enacting the environment and mission according to actual requirements of the fighter-bomber, the optimal trajectory of low altitude penetration is developed by use of studying, simulating and analyzing to improve the mission validity of the fighter-bomber. The simulation result for the optimal trajectory of the fighter-bomber shows that the optimal trajectory meets the demands, and testifies that the optimal method is effective and feasible.
出处
《飞行力学》
CSCD
北大核心
2008年第3期26-28,共3页
Flight Dynamics
关键词
低空突防
轨迹优化
仿真
low altitude penetration
trajectory optimization
simulation
