[1] 王永庆,罗云宝,王奇涛,等.面向机舰适配的舰载飞机起降特性分析[J].航空学报,2016,37(1):269-277.WANG Y Q,LUO Y B,WANG Q T,et al.Carrier suitability-oriented launch and recovery characteristics of piloted carrier-based aircraft[J].Acta Aeronautica et Astronautica Sinica,2016,37(1):269-277(in Chinese).
[2] 李晓磊,赵廷弟.基于模糊推理的舰载机进舰过程安全性仿真分析[J].航空学报,2013,34(2):325-333.LI X L,ZHAO T D.Carrier-based aircraft landing process safety simulation analysis based on fuzzy inference[J].Acta Aeronautica et Astronautica Sinica,2013,34(2):325-333(in Chinese).
[3] STEINBERG M.Development and simulation of an F/A-18 fuzzy logic automatic carrier landing system[C]//Second IEEE International Conference on Fuzzy Systems,1993.Piscataway,NJ:IEEE Press,1993:797-802.
[4] 张永花,周鑫.纵向甲板运动补偿技术研究[J].电光与控制,2012,19(4):18-22.ZHANG Y H,ZHOU X.Study on the longitudinal deck motion compensation technique[J].Electronics Optics & Control,2012,19(4):18-22(in Chinese).
[5] 张永花,周鑫.舰载机着舰点垂直运动补偿技术仿真研究[J].系统仿真学报,2013,25(4):826-830.ZHANG Y H,ZHOU X.Simulation study on landing point vertical motion in carrier landing[J].Journal of System Simulation,2013,25(4):826-830(in Chinese).
[6] 周鑫,彭荣鲲,袁锁中.舰载机理想着舰点垂直运动的预估与补偿[J].航空学报,2013,34(7):1663-1669.ZHOU X,PENG R K,YUAN S Z.Prediction and compensation for vertical motion of ideal touchdown point in carrier landing[J].Acta Aeronautica et Astronautica Sinica,2013,34(7):1663-1669(in Chinese).
[7] 满翠芳,江驹,王新华,等.舰载机动力补偿系统模糊逻辑设计技术[J].南京航空航天大学学报,2010,42(5):656-660.MAN C F,JIANG J,WANG X H,et al.Carrier-based aircraft approach power compensator system design based on fuzzy logic techniques[J].Journal of Nanjing University of Aeronautics & Astronautics,2010,42(5):656-660(in Chinese).
[8] 董然.ACLS纵向内回路控制系统研究[D].哈尔滨:哈尔滨工程大学,2013:56-61.DONG R.Research on the longitudinal inner loop configuration in ACLS[D].Harbin:Harbin Engineering University,2013:56-61(in Chinese).
[9] 张智,李佳桐,董然,等.针对舰艉流抑制的ACLS纵向控制律优化设计[J].哈尔滨工程大学学报,2016,37(6):802-811.ZHANG Z,LI J T,DONG R,et al.Optimal design on longitudinal automatic carrier landing system for carrier air wake rejection[J].Journal of Harbin Engineering University,2016,37(6):802-811(in Chinese).
[10] DAVID J M,ROBERT J W.军用规范——有人驾驶飞机的飞行品质(MIL-F-8785C)的背景资料和使用指南[M].李成忠,肖亚伦,方振平,等译.西安:飞行力学,1985:149-153.DAVID J M,ROBERT J W.Backgroud information and user guide for MIL-F-8785C,military specification-flying qualities of poloted airplanes[M].LI C Z,XIAO Y L,FANG Z P,et al translated. Xi'an:Flight Dynamics,1985:149-153(in Chinese).
[11] 杨一栋.舰载飞机着舰导引与控制[M].北京:国防工业出版社,2007:30-42.YANG Y D.Guidance and control of carrier aircraft landing[M]. Beijing:National Defend Industry Press,2007:30-42(in Chinese).
[12] 肖亚伦.飞行器运动方程[M].北京:航空工业出版社,1987:99-103.XIAO Y L.Motion equations of aerial vehicles[M].Beijing:Aeronautics Industry Press,1987:99-103(in Chinese).
[13] 肖亚伦,金长江.大气扰动中的飞行原理[M].北京:国防工业出版社,1993:99-101.XIAO Y L,JIN C J.Flight principle in atmospheric turbulence[M].Beijing:National Defend Industry Press,1993:99-101(in Chinese).
[14] KENNEDY J.Particle swarm optimization[M]//SAMMUT C,WEBB G I.Encyclopedia of machine learning.New York:Springer,2011:760-766.
[15] SCHUTTE J F,GROENWOLD A A.A study of global optimization using particle swarms[J].Journal of Global Optimization,2005,31(1):93-108.
[16] LIAO W,WANG J,WANG J.Nonlinear inertia weight variation for dynamic adaptation in particle swarm optimization[C]//International Conference in Swarm Intelligence. Berlin:Springer,2011:80-85.
[17] ANDERSON M R.Inner and outer loop manual control of carrier aircraft landing[C]//AIAA Guidance,Navigation and Control Conference.Reston:AIAA,1996:1-10.
[18] 许东松,刘星宇,王立新.航母运动对舰载飞机着舰安全性的影响[J].北京航空航天大学学报,2011,37(3):289-294.XU D S,LIU X Y,WANG L X.Influence of carrier motion on landing safety for carrier-based airplanes[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(3):289-294(in Chinese). |