推力矢量飞机控制系统设计与仿真研究  

Control System Design and Emulation for Vectored Thrust Aircraft

作　　者：王美仙[1] 李明[2] 张子军[1] 

机构地区：[1]沈阳飞机设计研究所飞行控制部,辽宁沈阳110035 [2]沈阳飞机设计研究所,辽宁沈阳110035

出　　处：《飞行力学》2007年第4期8-12,共5页Flight Dynamics

摘　　要：针对某型推力矢量飞机提出了一套控制方案,较好地将理论与工程实践结合起来,解决了飞机在全包线范围内的飞行控制问题。该控制方案包括常规机动控制器、大迎角超机动控制器、控制分配器及轨迹跟踪控制器等几个主要环节的设计,完成的控制系统满足全包线飞行品质的要求,可实现对大机动轨迹的精确跟踪。最后,对此综合控制系统进行数字仿真并给出部分仿真结果,结果表明所提出的飞行控制系统设计方案是成功的。For certain of vectored thrust aircraft, this paper introduces a set of control scheme which integrates theoretic with engineering practice well and solves the problems of full-envelope flight control. The scheme included the design of the following main controller： conventional maneuver controller, large angle super maneuver controller, control allocation mixer and trajectory tracking controller. The whole control system can fulfill the requests of full-envelope flying qualities and track the large maneuverable trajectory accurately. Finally, digital simulation for the control system was made and some simulating results were presented. The results show that the scheme of the flight control system is successful.

关 键 词：常规机动 大迎角超机动 控制分配 大机动轨迹跟踪 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]