CAJ | 학술논문

超机动飞机飞行控制和大迎角飞行品质研究，对于强调超机动能力的第四代战斗机的飞行控制律设计、验证和试飞评定有着重要意义。以鸭式布局飞机为研究对象，应用推力矢量技术，结合奇异摄动原理和逆系统理论，设计了基于非线性动态逆理论的超机动飞行控制律。从过失速状态飞机空气动力的非线性和非定常迟滞效应、大气紊流等方面初步验证了控制律的鲁棒性，并通过目标截获和跟踪任务的模拟，利用库珀一哈珀评定准则，对飞机的大迎角飞行品质进行了简要地分析。研究结果表明：设计的控制律对滞环和大气紊流的影响有较好的鲁棒性；飞机具有良好的大迎角截获和跟踪能力。研究结果可为超机动控制律设计与试飞验证提供一定的理论方法参考。
초궤동비궤비행공제화대영각비행품질연구，대우강조초궤동능력적제사대전두궤적비행공제률설계、험증화시비평정유착중요의의。이압식포국비궤위연구대상，응용추력시량기술，결합기이섭동원리화역계통이론，설계료기우비선성동태역이론적초궤동비행공제률。종과실속상태비궤공기동력적비선성화비정상지체효응、대기문류등방면초보험증료공제률적로봉성，병통과목표절획화근종임무적모의，이용고박일합박평정준칙，대비궤적대영각비행품질진행료간요지분석。연구결과표명：설계적공제률대체배화대기문류적영향유교호적로봉성；비궤구유량호적대영각절획화근종능력。연구결과가위초궤동공제률설계여시비험증제공일정적이론방법삼고。
It is important to study flight control and flight qualities at high angle of attack for flight control law design, verification and flight test assessment of the 4＇h generation aircraft, emphasized on super-maneuverability. Contrary to a canard aircraft, thrust vectoring technology, singular perturbation theory and inversion principle are applied to develop the post-stall control law based on the nonlinear dynamic inversion method. The robustness of the control law was verified in the following two aspects： nonlinear and unsteady hysteresis effect of aerodynamic in post-stall, atmospheric turbulence. The flight quality of this airplane is briefly assessed with the ＂Cooper-Harper＂ rating by ways of simulating target acquisition and tracking mission. The research results show that the robustness of the control law is well verified by the hysteresis of instrument and atmospheric turbulence and the aircraft has favorable ability of acquisition and tracking. This research can be a useful reference theoretically for the super-maneuverable flight control design and flight test.