Dynamics Analysis of Carrier-Based Aircraft with Off-Center Catapult Launch
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  • 英文篇名:Dynamics Analysis of Carrier-Based Aircraft with Off-Center Catapult Launch
  • 作者:ZHOU ; Jin ; ZHU ; Jianhui ; TONG ; Mingbo
  • 英文作者:ZHOU Jin;ZHU Jianhui;TONG Mingbo;School of Aeronautic Science and Engineering,Beihang University;College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics;
  • 英文关键词:carrier-based aircraft;;catapult launch;;off-center distance;;attitude angle;;landing gear
  • 中文刊名:NJHY
  • 英文刊名:南京航空航天大学学报(英文版)
  • 机构:School of Aeronautic Science and Engineering,Beihang University;College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics;
  • 出版日期:2019-06-15
  • 出版单位:Transactions of Nanjing University of Aeronautics and Astronautics
  • 年:2019
  • 期:v.36
  • 语种:英文;
  • 页:NJHY201903011
  • 页数:11
  • CN:03
  • ISSN:32-1389/V
  • 分类号:112-122
摘要
In order to enhance the safety of the catapult launch of the carrier-based aircraft,the catapult launch multibody dynamic model is established aiming at the problem of off-center catapult launch. The whole catapult process including four stages which are buffering,tensioning,releasing and taxiing is taken into consideration and the body dynamics of the off-center catapult during each stage is analyzed. The catapult launch dynamic differences between the conditions only considering taxiing and that considering four stages are compared,and the effects of the different initial off-center distances considering four stages on the attitude,landing gear load and acceleration of the carrier-based aircraft during catapult launch are discussed. The results show that only considering taxiing may underestimate the dynamics of the carrier-based aircraft substantially. When taking four stages into consideration,the initial off-center distance has small influence on the aircraft dynamic characteristics during buffering and tensioning but has larger influence on that during releasing and taxiing. The increase of the off-center distance will cause the enhancement of the aircraft rolling and yawing,which may lead to the load difference between the left and right landing gears and the increase of the aircraft lateral acceleration. The establishment and simulation of the catapult launch multi-body dynamic model founded on buffering,tensioning,releasing and taxiing provide reference for the carrier-based aircraft design and analysis of the catapult launch dynamics.
        In order to enhance the safety of the catapult launch of the carrier-based aircraft,the catapult launch multibody dynamic model is established aiming at the problem of off-center catapult launch. The whole catapult process including four stages which are buffering,tensioning,releasing and taxiing is taken into consideration and the body dynamics of the off-center catapult during each stage is analyzed. The catapult launch dynamic differences between the conditions only considering taxiing and that considering four stages are compared,and the effects of the different initial off-center distances considering four stages on the attitude,landing gear load and acceleration of the carrier-based aircraft during catapult launch are discussed. The results show that only considering taxiing may underestimate the dynamics of the carrier-based aircraft substantially. When taking four stages into consideration,the initial off-center distance has small influence on the aircraft dynamic characteristics during buffering and tensioning but has larger influence on that during releasing and taxiing. The increase of the off-center distance will cause the enhancement of the aircraft rolling and yawing,which may lead to the load difference between the left and right landing gears and the increase of the aircraft lateral acceleration. The establishment and simulation of the catapult launch multi-body dynamic model founded on buffering,tensioning,releasing and taxiing provide reference for the carrier-based aircraft design and analysis of the catapult launch dynamics.
引文
[1] SMALL D B. Full scale tests of nose tow catapulting[C]//1st AIAA Annual Meeting, Washington DC American Institute of Aeronautics and Astronautics.Bethpage,New York:AIAA,1964:78-85.
    [2] LUCAS C B. Catapult criteria for a carrier-based airplane:AD702814[R].[S.l.]:[s.n.],1968.
    [3] RAMSEY J,DIXON W. Carrier suitability tests of the model A-6A aircraft:ADA382399[R]. Maryland:Naval Air Test Center,1967:53-57.
    [4] YU H,NIE H. Dynamics analysis of carrier-based aircraft with off-center catapult launch[J]. Journal of Nanjing University of Aeronautics and Astronautics,2010,42(5):537-542.(in Chinese)
    [5] WU W H,SONG L T,ZHANG Y,et al. Analysis of factors affecting catapult launch of carrier aircraft and design of lateral control law[J]. Journal of Beijing University of Aeronautics and Astronautics,2019,45(4):662-671.
    [6] YU H,NIE H. Launch bar load analysis of carrierbased aircraft during off-center catapult launch[J]. Acta Aeronautica et Astronautica Sinica,2010,31(10):1953-1959.(in Chinese)
    [7] YU H,NIE H. Effects of off-center location on aircraft attitude during catapult launch[J]. Journal of Beijing University of Aeronautics and Astronautics,2011,37(1):10-14.(in Chinese)
    [8] ZHU Q D,LIU H,LI X L. Research on aircraft catapult in the case of different eccentricity[J]. Flight Dynamics,2016(2):10-14.(in Chinese)
    [9] LIN G F,HE Z D. Several problems during the ejection take-off process of sea-based aircraft[J]. Flight Dynamics,1991,9(3):31-39.(in Chinese)
    [10] WANG J Y,WU W H,GAO L,et al. Modeling and control of carrier-based airplane during catapult launch[J]. Aircraft Design,2010(2):10-13.(in Chinese)
    [11] HU M Q,BAI S G,CHEN Y R. Modeling and simulation for carrier-based aircraft catapult launch with six degrees of freedom[J]. Flight Dynamics,2013,31(2):97-100.(in Chinese)
    [12] WANG W J,QU X J,GUO L L. Multi-agent based hierarchy simulation models of carrier-based aircraft catapult launch[J]. Chinese Journal of Aeronautics,2008,21(3):223-231.
    [13] JIN C J,HONG G X. Dynamic problems of carrieraircraft catapult launching and arrest landing[J]. Acta Aeronautica et Astronautica Sinica,1990,11(12):534-542.
    [14] SU B,WANG D H. The effects of deck’s longitudinal shaking on launching performance[J]. Flight Dynamics,1993,11(3):61-66.(in Chinese)
    [15] JIA Z H,GAO Y,HAN W. Research on the limitation of vertical toss to the warship-based aircraft’s catapult-assisted take-off[J]. Flight Dynamics,2002,20(2):19-21.(in Chinese)
    [16] Naval Air Systems Commands. MIL-L-22589D Military specification:Launching system,nose gear type,aircraft[S].[S.l.]:[s.n],1991:15-16.
    [17] ZHANG Y M,WANG Q,LU Q S. Numerical analysis method for nonlinear dynamic equations of multibody systems with constraints[J]. Chinese Journal of Applied Mechanics,2002(3):54-58.
    [18] MA X T. Study on dynamic modeling and numerical algorithm of constrained multibody system[D]. Wuhan:Huazhong University of Science and Technology,2009.(in Chinese)
    [19] Aircraft Design Editorial Committee. Air-craft design manual:Take-off and landing system design[M]. Beijing:Aviation Industry Press,2002:202-203.(in Chinese)
    [20] Department of Defense Handbook. MIL-HDBK-2066(AS):Catapulting and arresting gear forcing functions for aircraft structural design[S].[S.l.]:[s.n],1999:46-48.
    [21] Naval Air Systems Commands. MIL-A-8863C(AS)Military specification:Airplane strength and rigidity ground for navy acquired airplanes[S].[S.l.]:[s.n],1993:4-5.
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