摘要
针对多飞行器协同作战的特点和要求,提出一种针对机动目标时间可控的协同制导律。该制导律由时间误差反馈与引入目标机动补偿的扩展比例导引(Augmented Proportional Navigation Guidance,APNG)结合推导得出,其结构形式简单,易于实现。通过多种目标机动形式数字仿真,验证新型制导律导引多飞行器在期望时间击中机动目标的有效性及可行性。
Based on the characteristics and requirement of synergistic combat, a time-controllable synergistic guidance law in attacking the maneuvering target is designed. The guidance law is deduced through a combination of time error feedback and augmented proportional navigation that includes target maneuvering compensation. The law is simple and convenient to be realized in engineering. Through digital simulations of multiple target maneuvering modes, the validity and feasibility of new guidance law are verified.
出处
《导弹与航天运载技术》
北大核心
2015年第1期92-95,共4页
Missiles and Space Vehicles
关键词
协同制导
目标机动
误差反馈
扩展比例导引
Cooperative guidance
Target maneuver
Feedback of the impact time error
Augmented Proportional NavigationGuidance
