1 |
A. E. Bryson and Y.-C. Ho, Applied Optimal Control, Wiley, New York, 1975.
|
2 |
A. E. Bryson, Linear feedback solution for minimum effort interception, rendezvous, and soft landing, AIAA J., 3(8) (1965), 1542-1544.
DOI
|
3 |
E. Kreindler, Optimality of proportional navigation, AIAA J., 11(6) (1973), 878-880.
DOI
|
4 |
H. Cho, Navigation constants in PNG law and the associated optimal control problems (in Korean), Proc. Korean Automatic Control Conference, Seoul, Korea, 1992, 578-583.
|
5 |
C. K. Ryoo, H. Cho, and M. J. Tahk, Time-to-go weighted optimal guidance with impact angle constraints, IEEE T. Contr. Syst. T., 14(3) (2006), 483-492.
DOI
ScienceOn
|
6 |
C. H. Lee, M. J. Tahk, and J. I. Lee, Generalized formulation of weighted optimal guidance laws with impact angle constraint IEEE T. Aero. Elec. Sys., 49(2) (2013), 1317-1312.
DOI
ScienceOn
|
7 |
M. Y. Ryu, C. H. Lee, and M. J. Tahk, New trajectory shaping guidance laws for anti-tank guided missile, P. I. Mech. Eng. G- J. Aer., 229(7) (2015), 1360-1368.
|
8 |
R. G. Cottrell, Optimal intercept guidance for short-range tactical missiles AIAA J., 9(7) (1971), 1414-1415.
DOI
|
9 |
C. K. Ryoo, H. Cho, and M. J. Tahk, Optimal guidance laws with terminal impact angle constraint, J. Guid. Contr. Dyn., 28(4) (2005), 724-732.
DOI
ScienceOn
|
10 |
M. J. Tahk, C. K. Ryoo and H. Cho, Recursive time-to-go estimation for homing guidance missiles, IEEE T. Aero. Elec. Sys., 38(1) (2002), 13-24.
DOI
ScienceOn
|
11 |
C. K. Ryoo, H. Cho, and M. J. Tahk, Closed-form solutions of optimal guidance with terminal impact angle constraints, Proceedings of the 2003 IEEE Int. Conf. Contr. Appl., Istanbul, Turkey, June 2003, 504-509.
|
12 |
C. K. Ryoo, H. S. Shin, and M. J. Tahk, Energy optimal waypoint guidance synthesis for anti-ship missiles, IEEE T. Aero. Elec. Sys., 46(1) (2010), 80-95.
DOI
ScienceOn
|
13 |
H. Cho, C. K. Ryoo, A. Tsourdos, and B. White, Optimal impact angle control guidance law based on linearization about collision triangle, J. Guid. Contr. Dyn., 37(3) (2014), 958-964.
DOI
ScienceOn
|
14 |
M. J. Tahk, B. M. Min, and H. C. Shim, Study on the time-to-go polynomial guidance (in Korean), Proc. Spring Conf. Korean Soc. Aero. Space Sci., Yong Pyong, Korea, (2007), 459-462.
|
15 |
C. H. Lee, T. H. Kim, M. J. Tahk, and I. H. Whang, Polynomial guidance laws considering terminal impact angle and acceleration constraints, IEEE T. Aero. Elec. Sys., 49(1) (2013), 74-92.
DOI
ScienceOn
|
16 |
T. H. Kim, C. H. Lee, M. J. Tahk, and I. S. Jeon, Augmented polynomial guidance with impact time and angle constraints, IEEE T. Aero. Elec. Sys., 49(4) (2013), 2806-2817.
DOI
ScienceOn
|
17 |
T. H. Kim, C. H. Lee, and M. J. Tahk, Time-to-go polynomial guidance with trajectory modulation for observability enhancement, IEEE T. Aero. Elec. Sys., 49(1) (2013), 55-73.
DOI
ScienceOn
|
18 |
Y. I. Lee, S. H. Kim, and M. J. Tahk, Optimality of linear time-varying guidance for impact angle control, IEEE T. Aero. Elec. Sys., 48(3) (2012), 2808-2817.
|
19 |
Y. I. Lee, S. H. Kim, and M. J. Tahk, Analytic solutions of optimal angular constrained guidance for first-order lag system, P. I. Mech. Eng. G- J. Aer., 227(3) (2013), 827-837.
|
20 |
Y. I. Lee, S. H. Kim, J. I. Lee, and M. J. Tahk, Analytic Solutions of Generalized Impact-Angle-Control Guidance Law for First-Order Lag System, J. Guid. Contr. Dyn., 36(1) (2013), 96-112.
DOI
ScienceOn
|
21 |
C. H. Lee, T. H. Kim, M. J. Tahk, Design of impact angle control guidance laws via high-performance sliding mode control, P. I. Mech. Eng. G- J. Aer., 227(2) (2013), 235-253.
|
22 |
I. S. Jeon and J. I Lee, Guidance law to reach circular target area with grazing angle constraint (in Korean), J. Soc. Aero. Space Sci., 36(9) (2008), 884-890.
|
23 |
B. G. Park, T. H. Kim, and M. J. Tahk, Optimal impact angle control guidance law considering the seeker's field-of-view limits, P. I. Mech. Eng. G- J. Aer., 227(8) (2013), 1347-1364.
|
24 |
I. S. Jeon, J. I. Lee, and M. J. Tahk, Impact-time-control guidance law for anti-ship missiles, IEEE T. Cont. Sys. Tech., 14(2) (2006), 260-266.
DOI
ScienceOn
|
25 |
J. I. Lee, I. S. Jeon, and M. J. Tahk, Guidance law to control impact time and angle, IEEE T. Aero. Elec. Sys., 43(1) (2007), 301-310.
DOI
ScienceOn
|
26 |
I. S. Jeon, J. I. Lee, and M. J. Tahk, Homing guidance law for cooperative attack of multiple missiles, J. Guid. Contr. Dyn., 33(1) (2010), 275-280.
DOI
ScienceOn
|
27 |
M. J. Tahk, B. K. Park, B. C. Sun, I. S. Hwang, H. J. Cho, and T. L. Song, The closed-form solution and its approximation of the optimal guidance law, 12th World Congress of IFAC, Sydney, Australia, July 1993, 207-210.
|
28 |
T. Kailath, Linear Systems,Prentice Hall, 1980.
|