|
|
- 2017
小型飞机自动着舰系统设计准则适用性分析
|
Abstract:
摘要 在进行自动着舰系统（ACLS）设计时，美军标AR-40A是目前较为常用的参考设计准则，但该准则的要求主要针对F/A-18等Ⅳ类飞机提出，并未说明在应用于Ⅰ类飞机自动着舰系统设计时的适用性。为研究AR-40A在Ⅰ类飞机自动着舰系统设计时的适用性，针对某型飞机及其尺寸缩比率为4的缩比机进行了全自动着舰系统设计。通过飞机-航母-大气环境综合仿真，选取着舰效果较好的全自动着舰系统设计结果，通过对其频域特性曲线分析对比，验证了AR-40A在Ⅰ类飞机自动着舰系统设计中的适用性。通过原型机、缩比机、F/A-18三者的频域特性对比，提出了AR-40A在应用于小型飞机自动着舰系统设计时应进行的低频段、中高频段划分及幅值、相角带宽频率等关键边界要求的修改建议，拓展了该准则的适用范围。
Abstract：US military standard AR-40A is a frequently used design principle when the automatic carrier landing system (ACLS) is designed. But the principle is mainly aiming at Class Ⅳ, such as F/A-18 and there is no instruction about whether the principle could be adapted in the Class Ⅰ aircraft. In order to explore its adaptability of AR-40A to ACLS of Class Ⅰ aircraft, the ACLS designs on both a certain airplane and its shrunk one with a shrinkage ratio of4 were carried out. A comprehensive simulation about shipboard aircraft, aircraft carrier and the atmospheric environment was done first, then the most satisfying ACLS design result was selected, and finally the frequency-domain characteristics of the results were analyzed and compared. The adaptability of AR-40A to ACLS of Class Ⅰ aircraft has been verified. Based on the comparison of frequency-domain characteristics among prototype aircraft, shrinkage aircraft and F/A-18, the paper proposes some adjustment advice of key border requirements, such as the amplitude bandwidth frequency and phase bandwidth frequency. Meanwhile, the low frequency band and the high frequency band should be categorized when using the ACLS design for the light plane. The effort may help to expand its application sphere.
| [1] | URNES J M,HESS R K,MOOMAW R F.H-dot automatic carrier landing system for approach control in turbulence[J].Journal of Guidance,Control,and Dynamics,1981,4(2):177-183. |
| [2] | 杨一栋.舰载机着舰引导技术译文集[M].北京:国防工业出版社,2004:73-84.YANG Y D.Translation of carrier-guided technology of shipboard[M].Beijing:National Defense Industry Press,2004:73-84(in Chinese). |
| [3] | RUDOWSKY T,HYNES M,LUTER M,et al.Review of the carrier approach criteria for carrier-based aircraft-Phase Ⅰ:Final report:NAWCADPAX/TR-2002/71[R].Maryland:Naval Air Warfare Center Aircraft Division Patuxent River,2002. |
| [4] | 陈孟钢,高金源.缩比模型飞机极其飞控系统与原型机的相似关系[J].飞行力学,2003,21(2):34-37.CHEN M G,GAO J Y.Similarity relationships between scaled-model aircraft with its flight control system and prototype aircraft[J].Flight Dynamics,2003,21(2):34-37(in Chinese). |
| [5] | SCHUST A P,YOUNG P N,SIMPSON W R.Automatic carrier landing system (ACLS) category Ⅲ certification manual:1506-01-1-2750[R].Annapolis:ARINC Research Corp.,1982. |
| [6] | 郭锁凤,申功璋,吴成富.先进飞行控制系统[M].北京:国防工业出版社,2003:214-218.GUO S F,SHEN G Z,WU C F.Advanced flight control system[M].Beijing:National Defense Industry Press,2013:214-218(in Chinese). |
| [7] | 杨一栋,郑峰婴,王新华.舰载机等效模型及着舰控制规范[M].北京:国防工业出版社,2013:5-18.YANG Y D,ZHENG F Y,WANG X H.Equivalent model of carrier-based aircraft and landing control specification[M].Beijing:National Defense Industry Press,2013:5-18(in Chinese). |
| [8] | 张明廉,徐军.舰载飞机自动着舰系统的研究[J].北京航空航天大学学报,1994,20(4):386-391.ZHANG M L,XU J.The research of automatic carrier-based aircraft landing system[J].Journal of Beijing University of Aeronautics and Astronautics,1994,20(4):386-391(in Chinese). |
| [9] | 章卫国,王新民,刘长林.舰载飞机纵向自动着舰控制系统研究[J].西北工业大学学报,1996,14(4):549-553.ZHANG W G,WANG X M,LIU C L.The research of longitudinal carrier-based aircraft automatic landing control system[J].Journal of Northwestern Polytechnical University,1996,14(4):549-553(in Chinese). |
| [10] | Department of Defense,US.Flying qualities of piloted aircraft:MIL-STD-1797A[S].Washington,D.C.:Department of Defense,US,1995. |
| [11] | 杨一栋.舰载飞机着舰引导与控制[M].北京:国防工业出版社,2007:105-106,188-195.YANG Y D.Guidance and control of carrier-based aircraft[M].Beijing:National Defense Industry Press,2007:105-106,188-195(in Chinese). |
| [12] | 杨一栋.着舰安全与复飞技术[M].北京:国防工业出版社,2013:33-36.YANG Y D.Landing and go-around technical security[M].Beijing:National Defense Industry Press,2013:33-36(in Chinese). |
| [13] | PRICKETT A L,PARKES C J.Flight testing of the F/A-18E/F automatic carrier landing system[C]//2001 IEEE Aerospace Conference.Piscataway,NJ:IEEE Press,2001:2593-2612. |
| [14] | BUTTRILL C S,ARBUCKLE P D,HOFFLER K D.Simulation model of a twin-tail,high performance airplane:NASA TM 107601[R].Hampton:Langley Research Center,1992. |
| [15] | 杨一栋.无人机着舰制导与控制[M].北京:国防工业出版社,2013:7-18.YANG Y D.Guidance and control of UAV carrier landing[M].Beijing:National Defense Industry Press,2013:7-18(in Chinese). |
| [16] | URNES J M,HESS R K.Development of the F/A-18A automatic carrier landing system[J].Journal of Guidance,Control,and Dynamics,1985,8(3):289-295. |
