摘要
根据机载布撒器的工作特点,设计了一种满足其作战要求的具有末端角度约束的制导律,并分析了工程实用性。采用基于视线角和视线角速度的最优滑模制导律,能够使得布撒器以合适的俯仰角和弹道倾角到达目标上方的开舱点,并进行抛撒子弹药。仿真结果表明,该制导律能够同时满足布撒器的命中精度和期望角度要求。
According to the performance of airborne dispenser, a guidance law with angle constraint which meets the requirements of it is designed, and its project feasibility is analyzed. Applying optimal sliding mode guidance law, based on the LOS （line-of-sight） angle and the LOS angular rates, the dispenser can reach the open-cabin-point upon the target with right pitch and trajectory dip angle, and cast sub-projectile. Simulation results show rhar the guidance law can meet the requirement of both precision and angle constraint of airborne dispenser.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第3期5-7,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
机载布撒器
末端角约束
制导律
airborne dispenser
terminal angle constraint
guidance law
