摘要
对攻击机本机照射激光束、投放激光制导炸弹的战术进行研究 ,即攻击机本机照射激光束、采用机翼非水平转弯投放方式投放激光制导炸弹、转弯退出的战术 .其关键点在于攻击机采用转弯退出战术把激光束连续地照射目标的战术要求和退出意图二者融合 .该战术由于采用机动投放和曲线退出战术方式 ,能够大大提高攻击机的生存力 .采用简化的攻击机质点模型 ,通过对攻击机转弯退出过程的分析 ,给出采用转弯退出战术的具体条件 .投放激光制导炸弹任务过程的数学仿真结果表明 ,所给出的条件能够满足攻击机本机照射激光束、投放激光制导炸弹、转弯退出的战术要求 .
The tactic to delivery guided bomb with laser is researched, while the laser bundle is transmitted by the fighter itself, that is to delivery guided bomb with laser in non wing level and to egress in turning. The major is to egress in turning, which synthesizes tactical requirement to shoot the target with the laser bundle and motive to egress. It can efficiently improve survival ability of the fighter to delivery bombs in maneuvering motion and to egress in curve. The condition to satisfy the two requirements is proposed with a simplified particle point model of the fighter and through analysis on the process that the fighter egresses in turning while continuously shoot the target with laser bundle. Simulations on the mission process prove that the proposed condition can satisfy the tactical requirements to delivery guided bomb with laser and to egress in turning while the fighter transmits laser bundle to shoot the target itself.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
2001年第1期40-43,共4页
Journal of Beijing University of Aeronautics and Astronautics