Time-optimal impact angle control for vertical plane engagements

IEEE Transactions on Aerospace and Electronic Systems

Volumn 35, Issue 2, 1999, Pages 738-742

  Lyul, Taek ^a   Sang, Song ^a   Shin, Jin ^a  

^a Hanyang University ERICA   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000922387     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.766954     Document Type: Article

References (7)

1. Kim, M., andGrider, K. V. (1973) Terminal guidance for impact attitude angle constrained flight trajectories. IEEE Transactions on Aerospace and Electronic Systems, AES-9, 6 (Dec. 1973), 852-859.
2. Song, T. L., Shin, S. J., and Cho, H. J. (1997) Impact angle control for planar engagements. In Proceedings of the 2nd ASCC, Seoul, July 1997, III 23-26.
3. Kirn, B. S., Lee, J. G., and Han, H. S. (1998) Biased PNG law for impact with angular constraint. IEEE Transactions on Aerospace and Electronic Systems, 34, 1 (Jan. 1998), 277-288.
4. Baba, Y., Takehira, T., and Takano, H. (1994) New guidance law for a missile with varying velocity. In Proceedings of the AIAA Guidance, Navigation, and Control Conference, Scottsdale, AZ, Aug. 1994, 207-215.
5. Song, T. L., and Um, T. Y. (1997) CLOS + IRTH composite guidance. IEEE Transactions on Aerospace and Electronic Systems, 33, 4 (Oct. 1997), 1339-1344.
6. Bryson, A. E., and Ho, Y (1975) Applied Optimal Control. New York: Wiley, 1975.
7. Siouris, G. M., and Leros, A. P. (1988) Minimum-time intercept guidance for tactical missiles. Control Theory and Advanced Technology, 4, 2 (June 1988), 251-263.