Impact Time Control with Generalized-Polynomial Range Formulation

[1]  Koray S. Erer,et al.  Impact Time and Angle Control Based on Constrained Optimal Solutions , 2016 .

[2]  Florian Holzapfel,et al.  Quartic range shaping for impact time control , 2017, 2017 25th Mediterranean Conference on Control and Automation (MED).

[3]  Youdan Kim,et al.  Modified Pure Proportional Navigation Guidance Law for Impact Time Control , 2016 .

[4]  Min-Jea Tahk,et al.  Nonsingular Sliding Mode Guidance for Impact Time Control , 2016 .

[5]  Youdan Kim,et al.  Lyapunov-based impact time control guidance laws against stationary targets , 2015, IEEE Transactions on Aerospace and Electronic Systems.

[6]  Min-Jea Tahk,et al.  Impact-Time-Control Guidance with Generalized Proportional Navigation Based on Nonlinear Formulation , 2016 .

[7]  Ilan Rusnak,et al.  Guidance of a homing missile via nonlinear geometric control methods , 1995 .

[8]  Shaul Gutman.  Impact-Time Vector Guidance , 2017 .

[9]  F. Holzapfel,et al.  Adaptive Impact Time Control Via Look-Angle Shaping Under Varying Velocity , 2017 .

[10]  Jin-Ik Lee,et al.  Impact-Time-Control Guidance Law With Constraints on Seeker Look Angle , 2017, IEEE Transactions on Aerospace and Electronic Systems.

[11]  N. A. Shneydor,et al.  Missile guidance and pursuit , 1998 .

[12]  Koray S. Erer,et al.  Switched-Gain Guidance for Impact Angle Control Under Physical Constraints , 2015 .

[13]  Ashwini Ratnoo,et al.  Lyapunov-Based Guidance Law for Impact Time Control and Simultaneous Arrival , 2016 .