Infrared and Laser Engineering, Volume. 47, Issue 3, 304004(2018)
Three-dimensional guidance law for missile of adjustable thrust with heat flux limit
[1] [1] 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] [2] 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] [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] [4] 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] [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] [6] Hughes R. Wielding a Bigger Stick: Western advances in BVRAAM capabilities [J]. Jane′s International Defence Review, 2016, 49(7): 50-55.
[7] [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] [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] [9] 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] [10] Wang Rui. Compound guided system with active laser imaging and passive infrared imaging [J]. Chinese Optics, 2013, 6(4): 536-543. (in Chinese)
[11] [11] 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] [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] [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] [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] [15] 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)
[17] [17] 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)
Get Citation
Copy Citation Text
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): 304004
Category: 红外技术及应用
Received: Oct. 10, 2017
Accepted: Nov. 20, 2017
Published Online: Apr. 26, 2018
The Author Email: Hongtao Wang (381094332@qq.com)