红外与激光工程, 2018, 47 (3): 0304004, 网络出版: 2018-04-26  

带热流密度限制的推力可控导弹三维制导律

Three-dimensional guidance law for missile of adjustable thrust with heat flux limit
作者单位
1 北京电子工程总体研究所, 北京 100854
2 中国长峰机电技术研究设计院, 北京 100854
引用该论文

王宏涛, 石德平, 刘恒军. 带热流密度限制的推力可控导弹三维制导律[J]. 红外与激光工程, 2018, 47(3): 0304004.

Wang Hongtao, Shi Deping, Liu Hengjun. Three-dimensional guidance law for missile of adjustable thrust with heat flux limit[J]. Infrared and Laser Engineering, 2018, 47(3): 0304004.

参考文献

[1] 陈阳, 储海荣, 郭立红. 捷联导引头积分比例导引制导精度[J]. 红外与激光工程, 2016, 45(6): 0631001.

    Chen Yang, Chu Hairong, Guo Lihong. Precision of integral proportion navigation guidance with strapdown seeker [J]. Infrared and Laser Engineering, 2016, 45(6): 0631001. (in Chinese)

[2] 臧路尧, 侯淼, 王辉, 等. 一种适用于红外制导弹药的变增益比例导引律[J]. 红外与激光工程, 2017, 46(5): 0504004.

    Zang Luyao, Hou Miao, Wang Hui, et al. A switched-gain proportional navigation applicable for infrared guidance munitions [J]. Infrared and Laser Engineering, 2017, 46(5): 0504004. (in Chinese)

[3] Wei X, Wang Y, Dong S, et al. A three-dimensional cooperative guidance law of multimissile system [J]. International Journal of Aerospace Engineering, 2015(4): 1-8.

[4] 叶继坤, 雷虎民, 赵岩, 等. 基于二阶滑模控制的微分几何制导律[J]. 系统工程与电子技术, 2017, 39(4): 837-845.

    Ye Jikun, Lei Humin, Zhao Yan, et al. Differential geometric guidance law based on second-order sliding control [J]. Systems Engineering and Electronic, 2017, 39(4): 837-845. (in Chinese)

[5] Li K B, Chen L, Bai X Z. Differential geometric modeling of guidance problem for interceptors [J]. Sci China Tech, 2011, 54(9): 2283-2295.

[6] Hughes R. Wielding a Bigger Stick: Western advances in BVRAAM capabilities [J]. Jane′s International Defence Review, 2016, 49(7): 50-55.

[7] Halswijk W. Online dynamic flight optimisation applied to guidance of a variable-flow ducted rocket [C]// AIAA Guidance, Navigation, and Control Conference, 2009: 1-14.

[8] Kingery J E, Ames F E. Stagnation region heat transfer augmentation at very high turbulence levels [J]. Journal of Turbomachinery, 2016, 138(8): 1-12.

[9] 关英姿. 整流罩气动加热对红外成像系统像质的影响[J].红外与激光工程, 2013, 42(2): 290-293.

    Guan Yingzi. Effort of pneumatic calefaction of the dome on IR imaging system quality [J]. Infrared and Laser Engineering, 2013, 42(2): 290-293. (in Chinese)

[10] 王锐. 激光红外主被动复合导引系统[J]. 中国光学, 2013, 6(4): 536-543.

    Wang Rui. Compound guided system with active laser imaging and passive infrared imaging [J]. Chinese Optics, 2013, 6(4): 536-543. (in Chinese)

[11] 李佳峰, 姜欢, 陈万春. 基于拟勒让德谱变换的防空导弹弹道优化[J]. 弹道学报, 2009, 21(3): 69-73.

    Li Jiafeng, Jiang Huan, Chen Wanchun. Midcourse trajectory optimization design for a surface-to-air missile based on legendre pseudospectral method [J]. Journal of Ballistics, 2009, 21(3): 69-73. (in Chinese)

[12] Ebrahimi B, Bahrami M, Roshanian J. Optimal sliding-mode guidance with terminal velocity constraint for fixed-interval propulsive maneuvers [J]. Acta Astronautica, 2008, 62(10):556-562.

[13] Justh E W, Krishnaprasad P S. Steering laws for motion camouflage [J]. Proceeding of the Royal Society A: Mathematical Physical and Engineering Science, 2005, 462(2076): 3629-3643.

[14] Reddy P V, Justh E W, Krishnaprasad P S. Motion camouflage in three dimensions [C]// IEEE Conference on Decision & Control, 2006: 13-15.

[15] 高长生, 李涧青, 荆武兴. 拦截机动目标的运动伪装制导律[J]. 宇航学报, 2016, 37(6): 737-743.

    Gao Changsheng, Li Jianqing, Jing Wuxing. Motion camouflage strategy guidance law for intercepting maneuvering target [J]. Journal of Astronautics, 2016, 37(6): 737-743. (in Chinese)

[16] 郭宁, 吕俊伟, 邓江生. 光电跟踪系统纯角度滤波器的设计[J]. 光学 精密工程, 2013, 21(7): 1818-1824.

    Guo Ning, Lv Junwei, Deng Jiangsheng. Design of filter only by angle information in opto-electronic tracking system [J]. Optics and Precision Engineering, 2013, 21(7): 1818-1824. (in Chinese)

[17] 李涧青. 远程空空导弹复合制导与控制研究[D]. 哈尔滨: 哈尔滨工业大学, 2014: 56-61.

    Li Jianqing. Study on compound guidance and control problems for long-range air to air missile [D]. Harbin: Harbin Institute of Technology, 2014: 56-61. (in Chinese)

王宏涛, 石德平, 刘恒军. 带热流密度限制的推力可控导弹三维制导律[J]. 红外与激光工程, 2018, 47(3): 0304004. Wang Hongtao, Shi Deping, Liu Hengjun. Three-dimensional guidance law for missile of adjustable thrust with heat flux limit[J]. Infrared and Laser Engineering, 2018, 47(3): 0304004.

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