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现代战机超机动攻击研究
引用本文:吴文海,耿昌茂,罗德林,沈春林.现代战机超机动攻击研究[J].南京航空航天大学学报,2004,36(4):417-421.
作者姓名:吴文海  耿昌茂  罗德林  沈春林
作者单位:1. 南京航空航天大学自动化学院,南京,210016;海军航空工程学院青岛分院,青岛,266041
2. 海军航空工程学院青岛分院,青岛,266041
3. 南京航空航天大学自动化学院,南京,210016
摘    要:在研究、比较两种非线性系统设计方法——动态逆和Backstepping的基础上,设计了具有大机动飞行的,基于Lyaponov全局稳定的Backstepping飞行控制律;其次,探讨了衡量机动攻击导引性能的评价尺度,并进一步研究了如何根据载机与目标的相对运动,导引载机机动飞行,以迅速满足载机空空导弹离轴发射条件,实现超机动攻击的导引律。最后,以攻击机动和非机动目标飞行仿真,说明了所研究的机动攻击导引方法的正确性和可行性。

关 键 词:战机  超机动攻击  发射条件  仿真分析
文章编号:1005-2615(2004)04-0417-05
修稿时间:2003年10月8日

Modern Fighter Study on PST-Attacking
WU Wen-hai.Modern Fighter Study on PST-Attacking[J].Journal of Nanjing University of Aeronautics & Astronautics,2004,36(4):417-421.
Authors:WU Wen-hai
Institution:WU Wen-hai~
Abstract:Post-stall technology (PST) aircraft has the capability of rapid nose pointing and the advantage of attacking the adversary air target. Based on the Backstepping method, a flight control law is designed, with which the modern fighter can be controlled to realize PST flight. Furthermore, a study on the attacking performance metric to measure combat advantage is presented; this has been used as a assessment for the design evaluation of the attacking guidance law, based on modern airborne missile, with capability of off-boresight launch. Simulation demonstrates that the designed guidance law is feasible in the guidance of fighter, aiming at the target rapidly and steadily.
Keywords:navigation guidance of fighter  post-stall technology  launching condition  simulation
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