Multi-objective Optimization of Aerodynamic Shape of Microspoiler for Spin-stabilized Projectile
QIAN Long1, CHANG Sijiang1, NI Yi2
(1.School of Energy and Power Engineering,Nanjing University of Science and Technology,Nanjing 210094,Jiangsu,China;2.Shanghai Institute of Mechanical and Electrical Engineering,Shanghai 201109,China)
[1] DYKES J,MONTALVO C,COSTELLO M,et al. Use of microspoilers for control of finned projectiles[J].Journal of Spacecraft and Rockets,2012,49(6):1131-1140. [2] SCHEUERMANN E,COSTELLO M,SILTON S,et al.Aerodynamic characterization of a microspoiler system for supersonic finned projectiles[J].Journal of Spacecraft and Rockets,2015,52(1):253-263. [3] FRESCONI F,COOPER G,CELMINS I,et al.Flight mechanics of a novel guided spin-stabilized projectile concept[J].Proceedings of the Institution of Mechanical Engineers,Part G.Journal of Aerospace Engineering ,2012,226(3):327-340. [4] CARETTE E,CAYZAC R,ZEIDLER M,et al. Innovative course correction devices:MANEGE Program[C]∥Proceedings of the 29th International Symposium on Ballistics.Edinburgh,UK:IBC,2016:29-39. [5] WEY P,MARTINEZ B,CAYZAC R,et al. 2D course correction system for spin-stabilized projectiles using a spoiler control surface[C]∥Proceedings of the 28th International Symposium on Ballistics.Atlanta,GA,US:IBC,2014:678-688. [6] FRESCONI F,PLOSTINS P.Control mechanism strategies for spin-stabilized projectiles[J].Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering,2010,224(9):979-991. [7] COSTELLO M,PETERSON A.Linear theory of a dual-spin projectile in atmospheric flight[J].Journal of Guidance, Control, and Dynamics,2000,23(5):789-797. [8] 王钰,王晓鸣,程杰,等.基于等效力方法的双旋弹侧向控制力落点响应分析[J].兵工学报,2016,37(8):1379-1387. WANG Y,WANG X M,CHENG J,et al.Analysis on impact point response of a dual-spin projectile with lateral force based on equi- valent force method[J].Acta Armamentarii,2016,37(8):1379-1387. (in Chinese) [9] BURCHETT B,COSTELLO M.Model predictive lateral pulse jet control of an atmospheric rocket[J].Journal of Guidance, Control,
and Dynamics,2002,25(5):860-867. [10] OLLERENSHAW D,COSTELLO M.Simplified projectile swerve solution for general control inputs[J].Journal of Guidance,Control,and Dynamics,2008,31(5):1259-1265. [11] ARNOULT G,ZEIDLER M,GARNIER E.Aerodynamic coefficient reconstruction of a controlled spin stabilized projectile using mono and multi fidelity surrogate models[C]∥Proceedings of the 31st International Symposium on Ballistics. Hyderabad,India:IBC,2019:764-775. [12] ARNOULT G,ZEIDLER M,GARNIER E.Optimization metho- dology for a 2-D course correction of a 155 mm spin-stabilized projectile[C]∥Proceedings of 2018 Applied Aerodynamics Conference. Atlanta,GA,US:AIAA,2018:1-21. [13] ARNOULT G,ZEIDLER M, GARNIER E.Control surface geo- metry surrogate-based optimization for spin-stabilized projectile course correction[J].AIAA Journal,2019,58(2):550-560. [14] 钱龙,刘丹,常思江.带微型扰流片旋转稳定弹气动特性分析[J].弹道学报,2020,32(3):61-69. QIAN L,LIU D,CHANG S J.Aerodynamic characteristics of a spin-stabilized projectile equipped with microspoiler[J].Journal of Ballistics,2020,32(3):61-69. (in Chinese) [15] 杨杰,刘丹,常思江.带微型扰流片旋转稳定弹外弹道建模与仿真[J].弹道学报,2020,32(4):7-13. YANG J,LIU D,CHANG S J.Modeling and simulation of external trajectory of spin-stabilized projectile with micro spoiler[J].Journal of Ballistics,2020,32(4):7-13.(in Chinese) [16] 杨杰,刘丹,常思江.带扰流片旋转稳定弹制导律研究[J].弹道学报,2021,33(1):65-70,96. YANG J,LIU D,CHANG S J. Research on guidance law of spin-stabilized projectile with spoiler[J].Journal of Ballistics,2021,33(1):65-70,96.(in Chinese) [17] DESPIRITO J,HEAVY K R. CFD computation of magnus moment and roll damping moment of a spinning projectile[C]∥Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit. Providence,RI,US:AIAA,2004.