航空学报 > 1993, Vol. 14 Issue (4): 159-168

先进武装直升机火控系统研究与仿真

孙隆和, 蔡若虹   

  1. 航空航天部电光设备研究所,洛阳 471009
  • 收稿日期:1991-01-03 修回日期:1991-09-14 出版日期:1993-04-25 发布日期:1993-04-25

STUDY AND SIMULATION OF FIRE CONTROL SYSTEM OF ADVANCED ARMED HELICOPTER

Sun Long-he, Cai Ruo-hong   

  1. The Electro-optical Equipment Research Institute, The Aerospace Ministry, Luoyang, 471009
  • Received:1991-01-03 Revised:1991-09-14 Online:1993-04-25 Published:1993-04-25

摘要: 提出了~套适合于武装直升机火控系统的设计方案,特点是采用两自度可动炮,大大地增大了火控系统攻击范围;采用飞行器状态估值器、目标状态估值器,提高了直升机的测量精度。采用闭环火控算法,大大地提高了射击精度。最后,利用蒙特卡洛法对整个火控系统进行了大量仿真,结果表明该火控系统与现有的武装直升机火控系统相比攻击范围大,射击精度高、反应快且具有较强的抗干扰能力,并能在机载计算机上实时工作。

关键词: 飞机火力控制, 仿真, 武装直升机, 脱靶量, 自校正控制

Abstract: The armed helicopter is an important weapon in the future war. It requires its fire control system with higher precision and faster reaction. In this paper, a design scheme suitable for gunship fire control system is put forwared. For this scheme, attack range can be increased by adopting two-degree-of-freedom trainable gun, measuring precision of airborne sensors about aircraft and target moving parameters can be raised by adopting aircraft state estimator and target state estimator, and hit probability can be raised by adopting closed loop fire control algorithm.The closed loop fire control system is one of the development orientations of the future fire control system.In this paper, a grey remnant difference self-tunning closed loop fire control algorithm is put forward. The mathematical model of the system is established and all algorithms are deduced.The simulation on the entire fire control system shows that this fire control system has large attack range, high hit probability, fast reaction velocity and excellent robustness and that this algorithm can perform real time operation on the airborne fire control computer.

Key words: aircraft fire control, simulation, miss distance, self--tunning control, gunship