摘要
为了满足综合系统多重递阶控制设计方法的需求 ,建立了空 -空航炮的机身指向火控解算方法。该方法是在期望弹丸命中目标的情况下求解机身期望指向及其变化率。在某验证机的控制增稳系统上 ,采用所建立的火控解算方法以及综合系统多重递阶控制设计方法 ,设计了综合飞行 /火力控制系统。仿真结果表明 ,所建立的空 -空航炮机身指向火控解算方法较好地满足了综合飞行 /火力控制系统的设计需求 。
The algorithm of the fire control system on the fuselage pointing is established to satisfy the requirement of designing the integrated control system on the multistage hierarchical control.It is to solve the expected fuselage pointing and the rate on the assumption of that the target could be hit.The algorithm is adopted in the method to design the integrated control system on the multistage hierarchical control to design the integrated flight/fire control(IFFC) system on the background fighter with the control augmented system.The simulation shows that the algorithm satisfies the requirement of the IFFC system well and the excellent dynamic performance of the IFFC system is attained.
出处
《火力与指挥控制》
CSCD
北大核心
2001年第3期14-16,23,共4页
Fire Control & Command Control
基金
航空科学基金资助项目
