CAJ | 학술논문

根据飞机刹车系统设计要求和系统的特点，提出飞机自动刹车系统总体框架。以自动刹车中止起飞（RTO）为例，对控制逻辑进行设计，利用Stateflow工具建立控制逻辑模型并进行仿真，仿真结果表明控制逻辑的正确性。建立自动刹车系统半物理仿真试验台，通过给定减速率3m/s2，对自动刹车系统进行全数字仿真和半物理仿真，全数字仿真得到飞机滑跑距离为672m，半物理仿真得到滑跑距离为1016m，减速率在2.88～3.07m/s2之间变化，均满足系统设计要求，验证了系统设计的正确性和合理性。
근거비궤찰차계통설계요구화계통적특점，제출비궤자동찰차계통총체광가。이자동찰차중지기비（RTO）위례，대공제라집진행설계，이용Stateflow공구건립공제라집모형병진행방진，방진결과표명공제라집적정학성。건립자동찰차계통반물리방진시험태，통과급정감속솔3m/s2，대자동찰차계통진행전수자방진화반물리방진，전수자방진득도비궤활포거리위672m，반물리방진득도활포거리위1016m，감속솔재2.88～3.07m/s2지간변화，균만족계통설계요구，험증료계통설계적정학성화합이성。
According to aircraft braking system design requirement and system characteristic, a aircraft automatic braking system whole frame was proposed. Taken automatic braking control logic of RTO state for example, control logic was designed, control logic model was set up and simulated using Statelfow, the simulation results show the correction of the control logic. The automatic braking system hardware-in-loop simulation was established. Through a given reduction rate of 3m/s2, the digital simulation and hardware-in-loop simulation were processed, results show that the taxiing distance of digital simulation was 672m, of hardware-in-loop simulation was 1016m, reduction rate changed between 2.88~3.07 m/s2, meet the requirment of system design, and its correctness and rationality is veriifed.