南京理工大学学报（自然科学版）
南京理工大學學報（自然科學版）
남경리공대학학보（자연과학판）
JOURNAL OF NANJING UNIVERSITY OF SCIENCE AND TECHNOLOGY
2014年
1期
83-88
,共6页
数字电子气动式%压力控制%比例积分微分控制%座舱
數字電子氣動式%壓力控製%比例積分微分控製%座艙
수자전자기동식%압력공제%비례적분미분공제%좌창
digital electronic-pneumatics%pressure control%proportion integration diffrentiation control%cabin
为改进数字气动式座舱控制系统的控制率,以典型运输机的座舱压力制度为控制目标,搭建模拟大气舱和模拟座舱组成的座舱压力控制系统性能测试台,开展数字气动式座舱控制系统的性能试验研究。根据系统比例积分微分( Proportion integration differentiation,PID)控制器各参数整定过程中所得试验结果与不同状态下座舱压力变化速率的变化规律,提出基于飞行状态模型下的座舱压力变化率优先控制方法,并进行了试验验证。试验结果表明：采用基于状态模型下的座舱压力变化率优先控制方法研制的数字电子气动式座舱压力控制系统,能够满足座舱压力制度及座舱变化速率的要求。
為改進數字氣動式座艙控製繫統的控製率,以典型運輸機的座艙壓力製度為控製目標,搭建模擬大氣艙和模擬座艙組成的座艙壓力控製繫統性能測試檯,開展數字氣動式座艙控製繫統的性能試驗研究。根據繫統比例積分微分( Proportion integration differentiation,PID)控製器各參數整定過程中所得試驗結果與不同狀態下座艙壓力變化速率的變化規律,提齣基于飛行狀態模型下的座艙壓力變化率優先控製方法,併進行瞭試驗驗證。試驗結果錶明：採用基于狀態模型下的座艙壓力變化率優先控製方法研製的數字電子氣動式座艙壓力控製繫統,能夠滿足座艙壓力製度及座艙變化速率的要求。
위개진수자기동식좌창공제계통적공제솔,이전형운수궤적좌창압력제도위공제목표,탑건모의대기창화모의좌창조성적좌창압력공제계통성능측시태,개전수자기동식좌창공제계통적성능시험연구。근거계통비례적분미분( Proportion integration differentiation,PID)공제기각삼수정정과정중소득시험결과여불동상태하좌창압력변화속솔적변화규률,제출기우비행상태모형하적좌창압력변화솔우선공제방법,병진행료시험험증。시험결과표명：채용기우상태모형하적좌창압력변화솔우선공제방법연제적수자전자기동식좌창압력공제계통,능구만족좌창압력제도급좌창변화속솔적요구。
This paper discusses the performance of the designed digital electro-pneumatic cabin pressure control system for a cabin pressure schedule of transport aircraft. For the purpose of this study,an experimental setup consisting of simulated hermetic cabin and altitude simulated chamber is configured for cabin pressure control system operation. A series of experimental tests are executed to evaluate the performance of cabin pressure control system. The parameters of proportional integration differentiation(PID) controller are optimized. In the optimization process,the variation regularity of the rate of cabin pressure change under various conditions is considered. An approach that makes the rate of cabin pressure change priority control based on the flight status model is proposed and verified experimentally. Experimental results show that the proposed approach can be adapted to the designed digital electro-pneumatic cabin pressure control system and that better cabin pressure schedule and rate of cabin pressure change can be obtained.
