| Citation: | WANG Bin, LEI Humin, LI Jiong, et al. Impact time control guidance law for large heading errors[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(3): 605-613. doi: 10.13700/j.bh.1001-5965.2017.0162(in Chinese)
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In order to achieve salvo attack for large heading errors with integrated time, an impact time control guidance (ITCG) law for large heading errors is proposed based on equivalent sliding mode control theory and Lyapunov stability theorem by adopting the nonlinear guidance equation and the time-to-go approximation algorithm according to predicting interception point (PIP). For stationary and non-maneuvering constant velocity targets, the proposed guidance law achieves impact time successfully with any designated initial heading error even when the closing speed is negative. Initial conditions of the missile guidance are widely broadened. Rigorous theoretical proof demonstrates the validity of the guidance law. The simulation results under different initial conditions verify the effectiveness of the proposed guidance law.
| [1] |
KIM B S, LEE J G, HAN H S.Biased PNG law for impact with angular constraint[J].IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(1):277-288. doi: 10.1109/7.640285
|
| [2] |
张友安, 马国欣.攻击时间控制的动态逆三维制导律[J].哈尔滨工程大学学报, 2010, 31(2):215-219. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgcdxxb201002014
ZHANG Y A, MA G X.Dynamic inversion three-dimensional guidance law for impact time control[J].Journal of Harbin Engineering University, 2010, 31(2):215-219(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgcdxxb201002014
|
| [3] |
张友安, 张友根.多导弹攻击时间与攻击角度两阶段制导[J].吉林大学学报(工学版), 2010, 40(5):1442-1447. http://or.nsfc.gov.cn/bitstream/00001903-5/101415/1/1000000735946.pdf
ZHANG Y A, ZHANG Y G.Two stages guidance to control impact time and impact angle for multi-missiles[J].Journal of Jilin University(Engineering and Technology Editiion), 2010, 40(5):1442-1447(in Chinese). http://or.nsfc.gov.cn/bitstream/00001903-5/101415/1/1000000735946.pdf
|
| [4] |
HARL N, BALAKRISHNAN S.Impact time and angle guidance with sliding mode control[J]. IEEE Transactions on Control Systems Technology, 2012, 20(6):1436-1449. doi: 10.1109/TCST.2011.2169795
|
| [5] |
LEE J I, JEON I S, TAHK M J.Guidance law to control impact time and angle[J].IEEE Transactions on Aerospace and Electronic Systems, 2007, 43(1):301-310. doi: 10.1109/TAES.2007.357135
|
| [6] |
ARITA S, UENO S. Optimal feedback guidance for nonlinear missile model with impact time and angle constraints[C]//AIAA Guidance, Navigation, and Control(GNC)Conference. Reston: AIAA, 2013: 1-12.
|
| [7] |
ZHANG L M, SUN M W, CHEN Z Q, et al.Receding horizon trajectory optimization with terminal impact specifications[J].Mathematical Problems in Engineering, 2014, 28(6):1-8. https://www.hindawi.com/journals/mpe/2014/604705/tab2/
|
| [8] |
YAN F, KEMAO M, YUQING C.Cooperative guidance laws with constraints on impact time and terminal angle[J].Journal of System Simulation, 2014, 26(10):2434-2441. https://www.researchgate.net/publication/289645580_Cooperative_guidance_laws_with_constraints_on_impact_time_and_terminal_angle
|
| [9] |
马国欣, 张友安.带有导引头视场限制的攻击时间控制导引律[J].弹道学报, 2013, 25(2):6-11. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=ddxb201302002
MA G X, ZHANG Y A.Impact time control guidance law with seeker field-of-view limit[J].Journal of Ballistics, 2013, 25(2):6-11(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=ddxb201302002
|
| [10] |
ZHANG Y A, MA G X, LIU A L.Guidance law with impact time and impact angle constraints[J].Chinese Journal of Aeronautics, 2013, 26(4):960-966. doi: 10.1016/j.cja.2013.04.037
|
| [11] |
GHOSH S, GHOSE D, RAHA S. Three dimensional retro-PN based impact time control for higher speed non-maneuvering targets[C]//2013 IEEE 52nd Annual Conference on Decision and Control(CDC). Piscataway, NJ: IEEE Press, 2013: 4865-4870.
|
| [12] |
KUMAR S R, GHOSE D. Sliding mode control based guidance law with impact time constraints[C]//2013 American Control Conference(ACC). Piscataway, NJ: IEEE Press, 2013: 5760-5765.
|
| [13] |
JEON I S, LEE J I, TAHK M J.Homing guidance law for cooperative attack of multiple missiles[J].Journal of Guidance, Control, and Navigation, 2010, 33(1):275-280. doi: 10.2514/1.40136
|
| [14] |
马国欣, 张友安, 李大鹏.基于虚拟领弹的攻击时间和攻击角度控制[J].飞行力学, 2009, 27(5):51-54. http://d.wanfangdata.com.cn/Periodical_fxlx200905014.aspx
MA G X, ZHANG Y A, LI D P.Virtual-leader based impact time and impact angle control[J].Flight Dynamics, 2009, 27(5):51-54(in Chinese). http://d.wanfangdata.com.cn/Periodical_fxlx200905014.aspx
|
| [15] |
SHIYU Z, RUI Z, CHEN W, et al.Design of time-constrained guidance laws via virtual leader approach[J].Chinese Journal of Aeronautics, 2010, 23(1):103-108. doi: 10.1016/S1000-9361(09)60193-X
|
| [16] |
KIM T H, LEE C H, JEON I S, et al.Augmented polynomial guidance with impact time and angle constraints[J].IEEE Transactions on Aerospace and Electronic Systems, 2013, 49(4):2806-2817. doi: 10.1109/TAES.2013.6621856
|
| [17] |
李辕, 赵继广, 白国玉, 等.基于预测碰撞点的剩余飞行时间估计方法[J].北京航空航天大学学报, 2016, 42(8):1667-1674. http://bhxb.buaa.edu.cn/CN/abstract/abstract13404.shtml
LI Y, ZHAO J G, BAI G Y, et al.The method of time-to-go estimation based on predicted crack point[J].Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8):1667-1674(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract13404.shtml
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