[1] SARAH N D, NESRIN S K. Survey of planetary entry guidance algorithms[J]. Progress in Aerospace Sciences, 2014, 68(1):22-28. [2] 冉茂鹏, 王青, 莫华东, 等. 基于自适应神经模糊系统的高超声速飞行器再入预测制导[J]. 兵工学报, 2014, 35(12):2016-2022. RAN M P, WANG Q, MO H D, et al. ANFIS-based predictive reentry guidance for hypersonic vehicles[J]. Acta Armamentarii, 2014, 35(12):2016-2022. (in Chinese) [3] 赵汉元. 飞行器再入动力学与制导[M]. 长沙: 国防科技大学出版社, 1997. ZHAO H Y. Spacecraft reentry dynamics and guidance[M]. Changsha: National University of Defense Technology Press, 1997.(in Chinese) [4] LU P. Entry guidance: a unified method[J]. Journal of Guidance Control and Dynamics, 2014, 37(3):713-728. [5] SPRATLIN K M. An adaptive numeric predictor-corrector gui- dance algorithm for atmospheric entry vehicles[R]. Cambridge, MA, US: Massachusetts Institute of Technology, 1987. [6] XUE S, LU P. Constrained predictor-corrector entry guidance [J]. Journal of Guidance Control and Dynamics, 2010, 33(4): 1273-1281. [7] CHENG L, WANG Z B, CHENG Y, et al. Multi-constrained predictor-corrector reentry guidance for hypersonic vehicles[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232(61):3049-3067. [8] 赵江, 周锐. 基于倾侧角反馈控制的预测校正再入制导方法[J]. 兵工学报, 2015, 36 (5):823-830. ZHAO J, ZHOU R. Predictor corrector reentry guidance based on feedback bank angle control[J]. Acta Armamentarii, 2015, 36(5): 823-830.(in Chinese) [9] WANG H L, LI Q D, REN Z. Predictor-corrector entry guidance for high-lifting hypersonic vehicles[C]∥Proceedings of the 35th Chinese Control Conference.Chengdu, China: IEEE Technical Committee on Control Theory,Chinese Association of Automation, 2016: 5636-5640.
[10] 程阳, 程林, 张庆振, 等. 基于在线约束限制的飞行器预测校正制导[J]. 北京航空航天大学学报, 2017, 43(10): 2143-2153. CHENG Y, CHENG L, ZHANG Q Z, et al. Aircraft predictor-corrector guidance based on online constraint limit enforcement[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 2143-2153.(in Chinese) [11] 水尊师, 周军, 葛致磊. 基于高斯伪谱方法的再入飞行器预测校正制导方法研究[J]. 宇航学报, 2011, 32(6):1249-1255. SHUI Z S, ZHOU J, GE Z L. On-line predictor-corrector gui- dance based on Gauss pseudospectral method[J]. Journal of Astronautics, 2011, 32(6):1249-1255.(in Chinese) [12] 王青, 莫华东, 吴振东, 等. 基于能量的高超声速飞行器再入混合制导方法 [J]. 北京航空航天大学学报, 2014, 40(5): 579-584. WANG Q, MO H D, WU Z D, et al. Energy based hybrid reentry guidance for hypersonic vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(5):579-584.(in Chinese) [13] LU P, BRUNNER C W, STACHOWIAK S J, et al. Verification of a fully numerical entry guidance algorithm[J]. Journal of Guidance, Control, and Dynamics, 2016, 40(2): 230-247. [14] FU W X, LIU D K, CHEN K, et al. An improved predictor-corrector entry guidance method for hypersonic flight vehicle[J]. Advances in Mechanical Engineering, 2017, 9(10): 1-9. [15] 胡正东, 郭才发, 蔡洪. 天基对地打击动能武器再入解析预测制导技术[J].宇航学报, 2009, 30(3): 1039-1044. HU Z D, GUO C F, CAI H. Analytical predictive guidance for space-to-ground kinetic weapon in reentry[J]. Journal of Astronautics, 2009, 30(3): 1039-1044.(in Chinese) [16] 崔乃刚, 黄荣, 傅瑜, 等. 基于匹配渐进展开的跳跃式再入解析预测-校正制导律设计[J]. 航空学报, 2015, 36(8): 2764-2772. CUI N G, HUANG R, FU Y, et al. Design of analytical prediction-correction skip guidance law based on matched asymptotic expansions[J]. Acta Aeronautical et Astronautica Sinica, 2015, 36(8): 2764-2772.(in Chinese) [17] KLUEVER C A. Entry guidance using analytical atmospheric skip trajectories[J]. Journal of Guidance, Control, and Dynamics, 2008, 31(5): 1531-1535. [18] 胡锦川, 张晶, 陈万春. 高超声速飞行器平稳滑翔弹道解析解及其应用[J]. 北京航空航天大学学报, 2016, 42(5):961-968. HU J C, ZHANG J, CHEN W C. Analytical solutions of steady glide trajectory for hypersonic vehicle and planning application[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(5):961-968.(in Chinese) [19] LI H F, ZHANG R, LI Z Y, et al. New method to enforce inequality constraints of entry trajectory[J]. Journal of Guidance, Control, and Dynamics, 2012, 35(5): 1662-1667. [20] 曾宪法, 王洁瑶, 王小虎. 基于能量和解析预测校正的滑翔制导[J]. 系统工程与电子技术, 2013, 35(12): 2582-2588. ZENG X F, WANG J Y, WANG X H. Gliding guidance based on energy and analytical predictor corrector[J]. Systems Engineering and Electronics, 2013, 35(12):2582-2588.(in Chinese) [21] LIU S Y, LIANG Z X, LI Q D, et al. Predictor-corrector guidance for entry with terminal altitude constraint[C]∥Proceedings of the 35th Chinese Control Conference. Chengdu, China:IEEE Technical Committee on Control Theory,Chinese Association of Automation, 2016: 5557-5562. [22] SHEN Z J, LU P. Onboard generation of three-dimensional constrained entry trajectories[J]. Journal of Guidance Control and Dynamics, 2003, 26(1): 111-121. [23] 张鹏, 都延丽, 项凯. 高升阻比RLV的约束预测校正再入制导[J].飞行力学, 2018(3):70-74. ZHANG P, DU Y L, XIANG K. Constrained predictive-corrector entry guidance for high lift-to-drag RLV[J]. Flight Dynamics, 2018(3):70-74. (in Chinese) [24] LIANG Z X, REN Z, LI Q D. Evolved atmospheric entry corridor with safety factor[J]. Acta Astronautica, 2018, 143: 82-91. [25] LU P. Entry guidance using time-scale separation in gliding dynamics[J]. Journal of Spacecraft and Rockets, 2015, 52(4):1253-1258. [26] RICHIE G. The common aero vehicle: space delivery system of the future[C]∥Proceedings of the AIAA Space Technology Conference and Exposition. Albuquerque, NM, US: AIAA, 1999. [27] 王光伦. 高超声速飞行器再入段预测校正制导研究[D]. 哈尔滨: 哈尔滨工业大学, 2010. WANG G L. Predictor-corrector reentry guidance for hypersonic vehicles[D]. Harbin: Harbin Institute of Technology, 2010.(in Chinese)
第40卷第1期 2019 年1月兵工学报ACTA ARMAMENTARIIVol.40No.1Jan.2019
|