CAJ | 학술논문

为了探索出一条适合于评估失速迎角前大迎角飞行品质评估的思路，通过选取推杆并改变 10°姿态角，带过载的从一侧到另一侧的倾斜并截获90°滚转角及空-空跟踪三项任务作为子任务集，在一台地面飞行模拟器上对一架第三代战斗机大迎角飞行品质进行了评估，并把评估结果与通过等效系统方法得到的结果进行了对比，结果表明尽管大迎角品质边界相对于小迎角有所不同，但只要适当调整品质边界，则用于评估小迎角品质的方法如等效系统等，在大迎角时仍可采用。
위료탐색출일조괄합우평고실속영각전대영각비행품질평고적사로，통과선취추간병개변 10°자태각，대과재적종일측도령일측적경사병절획90°곤전각급공-공근종삼항임무작위자임무 집，재일태지면비행모의기상대일가제삼대전두궤대영각비행품질진행료평고，병파평고결과여통 과등효계통방법득도적결과진행료대비，결과표명진관대영각품질변계상대우소영각유소불동，단 지요괄당조정품질변계，칙용우평고소영각품질적방법여등효계통등，재대영각시잉가채용。
In order to explore how to evaluate the high attack(AOA) flying qualities before stall AOA,through pushing stick and changing posture angle by 10°, to roll from bank to bank and to capture 90° rollangle and air to air tracking are chosen as a subset to study flying qualities at high angle of attak. Second-ly, flying qualities of a third generation fighter are evaluated with a simulator. At last, the results of simu-lation evaluation are compared with ones derived from equivalent system method. The conclusion is that ifthe boundary of flying qualities are adjusted suitably, the high AOA flying qualities can still be evaluatedby equivalent system method, although the boundary of high AOA flying qualities is different from smallAOA ones.