AEROSPACE SHANGHAI, Volume. 41, Issue 5, 145(2024)
Missile-target Dynamic Allocation Method Based on Neural Network Residual Time Estimation
[11] Y P LU, D Z CHEN. A new exact algorithm for the weapon-target assignment problem. Omega, 98, 102138(2019).
[14] D GIBBONS, C C LIM, P SHI. Deep learning for bipartite assignment problems, 2318-2325(2019).
[17] Z R BOGDANOWICZ. A new efficient algorithm for optimal assignment of smart weapons to tar-gets. Computers& Mathematics with Applications, 58, 1965-1969(2009).
[18] Z F LI, X M LI, J J DAI et al. Sensor-weapon-target assignment based on improved SWT-opt algorithm, 25-28(2011).
[19] D B DONG, Y H ZHU, Z Z DU et al. Multi-target dynamic hunting strategy based on improved K-means and auc-tion algorithm. Information Sciences, 640, 119072(2023).
[21] P ZARCHAN. Tactical and strategic missile guidance(2012).
[22] M J TAHK, C K RYOO, H CHO. Recursive time-to-go estimation for homing guidance missiles. IEEE Transactions on Aerospace and Electronic Systems, 38, 13-24(2002).
[23] I JEON, J LEE, M TAHK. Impact-time-control guidance law for anti-ship missiles. IEEE Transactions on Control Systems Technology, 14, 260-266(2006).
[24] C K RYOO. Optimal guidance laws with terminal impact angle constraint. Journal of Guidance,Control,and Dynamics, 28, 724-732(2005).
[25] T H KIM, C H LEE, I S JEON et al. Augmented polynomial guidance with impact time and angle constraints. IEEE Transactions on Aerospace and Electronic Systems, 49, 2806-2817(2013).
[26] P LIU, R SUN, W LI. Homing guidance law with falling angle and flying time control. Journal of Harbin Institute of Technology, 21, 55-61(2014).
[30] J T L RIGGS. Linear optimal guidance for short range air-to-air missile, 757-764(1979).
[31] N DHANANJAY, D GHOSE. Accurate time-to-go estimation for proportional navigation guidance. Journal of Guidance,Control,and Dynamics, 37, 1378-1383(2014).
[32] Y A ZHANG, G X MA, H L WU. A biased proportional navigation guidance law with large impact angle constraint and the time-to-go estimation. Proceedings of the Institution of Mechanical Engineers,Part G:Journal of Aerospace Engineering, 228, 1725-1734(2014).
Get Citation
Copy Citation Text
Shi SU, Ying NAN, Mingyong HE. Missile-target Dynamic Allocation Method Based on Neural Network Residual Time Estimation[J]. AEROSPACE SHANGHAI, 2024, 41(5): 145
Category: Innovation and Exploration
Received: Oct. 24, 2023
Accepted: --
Published Online: Jan. 15, 2025
The Author Email: